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Information Flux Theory: A Reinterpretation of the Standard Model with a Single Fermion and the Origin of Gravity

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02 September 2025

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03 September 2025

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Abstract
Background:The Standard Model (SM) has been successful, yet it fails to explain the origin of fermion masses and mixing parameters. Methods: In this study we construct the single-fermion framework “Information Flux Theory (IFT),” derived from the Unified Evolution Equation. IFT preserves gauge symmetry while replacing Standard Model fields with a single fundamental operator, yielding analytic solutions without adjustable parameters. Results: IFT reproduces all SM particle masses—including the 125 GeV Higgs mass—and the CKM matrix within current experimental precision, requiring neither additional particles nor fine-tuning. Conclusion: These results demonstrate that IFT can fully replace the Standard Model with a single-fermion description, providing a conceptually simpler yet phenomenologically complete foundation for particle physics. Supplement: This paper includes proofs for two Clay Millennium Problems: the Yang–Mills mass gap and the Navier–Stokes equations. Note Added: Furthermore, as a result of this series of studies, the origin of gravity has now been clarified.
Keywords: 
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1. Introduction

1.1. Status of the Standard Model and Open Questions

1.1.1. Achievements

The Standard Model (SM), established in the 1970s, is built on the gauge symmetry SU ( 3 ) C SU ( 2 ) L U ( 1 ) Y and spontaneous symmetry breaking via the Higgs mechanism. Through (1) precision tests of electroweak interactions at LEP/SLC, (2) the consistent running of parameters such as α s ( M Z ) and sin 2 θ W , and (3) the complete observation of the particle spectrum—including the discovery of the Higgs boson in 2012— it has almost entirely covered the phenomenology in the 100 GeV– 10 TeV range[219]. Theoretically, it functions as a well-defined perturbative quantum field theory thanks to (i) a strictly fixed interaction structure enforced by local gauge symmetry, (ii) a commutative operator algebra on four-dimensional commutative spacetime, and (iii) the fulfillment of anomaly-cancellation conditions. Consequently, it enjoys exceptionally high experimental credibility, as demonstrated by the 10 10 precision of quantum electrodynamics and the unitarity tests of the CKM matrix in flavour physics.

1.1.2. Outstanding Problems

From the viewpoints of parameter minimality and an origin-based explanation, the SM leaves the following fundamental issues unresolved:
1. 
Origin of fermion masses and mixings The Yukawa matrices Y f contain 13 mass parameters and 10 mixing parameters; their hierarchical structure (e.g. m t / m u 10 5 ) and the texture of the CKM matrix are not fixed intrinsically but must be supplied externally.
2. 
Neutrino masses and CP phases The SM predicts strictly massless neutrinos, yet oscillation experiments show Δ m i j 2 0 . Whether neutrinos are Majorana or Dirac particles and the origin of lepton CP violation remain open questions[231].
3. 
Stability and naturalness of the scalar sector The Higgs mass is quadratically sensitive to radiative corrections (the hierarchy problem); stabilisation up to Λ Pl demands a dedicated mechanism.
4. 
The strong-CP problem The experimental requirement θ QCD < 10 10 is not naturally accommodated within the SM.
5. 
Consistency with gravitational and cosmological phenomena Cosmological observables such as dark matter, dark energy, and inflation are inadequately explained by SM+GR alone, calling for unification at the quantum-gravity scale.
6. 
Multiplicity of free parameters and aesthetic concerns The O ( 20 ) free parameters of the SM violate the principle of theoretical minimality, and the search for a more fundamental reduction principle is ongoing.

1.1.3. Position of the Present Work

The Information Flux Theory (IFT) proposed here aims to resolve these outstanding issues by
  • simultaneously describing all fermion families with a single fermion operator, automatically generating the Yukawa matrices via an exponential rule and operator contraction;
  • reproducing masses, mixings, and the Higgs sector without additional parameters while explicitly preserving the gauge group SU ( 3 ) C SU ( 2 ) L U ( 1 ) Y ;
  • introducing a Unified Evolution Equation as the foundational equation, naturally extendable to gravitational and cosmological terms.
In this way, IFT seeks to preserve the successes of the SM while simultaneously resolving the fundamental problems (i)–(vi) in one stroke. This section organises the achievements and limitations of the SM, and the construction of IFT is developed in the following sections.

1.2. Conceptual Basis of Information Flux Theory

1.2.1. Core Idea—A Single Fermion and Self-Information Flux

All observable quantities in the universe can be reduced to the conserved 4-vector
J μ ( x ) : = Ψ ¯ ( x ) γ μ Ψ ( x ) , μ J μ = 0 ,
namely the self-information flux of a single fermion Ψ. Here Ψ is the unique field in the fundamental representation of SU ( 3 ) C × SU ( 2 ) L × U ( 1 ) Y . “Generations’’ are replaced by a series of projectors Ψ n = Π n Ψ with Π n 2 = Π n and Π m Π n = 0 ( m n ) , while the mass hierarchy is fixed by an exponential rule  m n ε n ( ε : information-dissipation rate). The Yukawa matrices are not inputs but outcomes, drastically reducing the free constants of the Standard Model.

1.2.2. Unified Evolution Equation (UEE)

The time evolution of the information flux obeys the Lindblad (GKLS) equation
ρ ˙ = i [ H , ρ ] + α L α ρ L α 1 2 { L α L α , ρ } ,
such that in the IR limit H H GR it coincides with the Einstein–Hilbert action, while in the UV limit H H SM , thereby linking quantum theory and gravity through a single principle.

1.2.3. Masses and Mixings from Minimal Degrees of Freedom

With dissipators chosen as L α γ Π n Ψ Π m ( γ : dissipation coefficient), mass generation and mixing are induced automatically through the contractions of Π n . Because the construction employs only the gauge-covariant derivative D μ = μ i g a A μ a T a , symmetry is preserved.

1.2.4. Methodological Outline

The theory is developed through:
(i)
a rigorous derivation of the UEE and anomaly-cancellation conditions,
(ii)
deduction of exponential-rule Yukawa matrices from the projector series,
(iii)
comparison of the dissipation rate ε with experimental data
and consequently shown to reproduce the Standard Model in its entirety.

1.3. Unified Evolution Equation and Construction Method of the Single-Fermion Framework

1.3.1. Design Principle—Coexistence of Conservation and Dissipation

This theory is founded on the dual principle that “local gauge quantities are conserved, yet environmental dissipation organises the system.” The dynamics of the density operator ρ ( t ) are given by
ρ ˙ = i [ H , ρ ] + α L α ρ L α 1 2 { L α L α , ρ }
of GKLS type. The trace ρ = 1 is strictly conserved, while the von Neumann entropy satisfies S ˙ ( ρ ) = 1 2 α [ L α , L α ] ρ 0 , explicitly manifesting time irreversibility.

1.3.2. Minimal Building Blocks

Field operators are placed in H tot = H Mink H int , and only the gauge-covariant derivative D μ = μ i g a A μ a T a is employed. The effective Hamiltonian is
H = d 3 x Ψ ¯ i γ 0 γ j D j Ψ + H gauge ,
with no mass term at the outset; masses are generated automatically by the projector contractions described below.

1.3.3. Single Fermion and Projector Series

The 12 SM fermions are unified into a single Dirac operator Ψ . “Generations’’ are represented by the projector series
Ψ n = Π n Ψ , Π n 2 = Π n , Π m Π n = 0 ( m n ) .
Choosing the dissipators as L α γ Π n Ψ Π m , one induces the exponential rule m n = m 0 ε n , ε = γ / Λ , so that the Yukawa matrices are determined as a consequence of ε .

1.3.4. Construction Algorithm (Outline)

1) 
Anomaly Cancellation: Impose α [ T a , L α ] = 0 to fix the gauge representations identical to those of the SM.
2) 
Projector Contraction: Use Π m Ψ Π n = δ m n Ψ n to derive the exponential-rule Yukawa matrices.
3) 
RG Consistency: Require β g = 0 , β ε = 0 to reproduce α s ( M Z ) and sin 2 θ W within experimental accuracy.
4) 
Gravitational Limit: Add L grav γ G R Ψ and recover the Einstein equation in the IR.
The following chapters rigorously formalise each of these steps and perform detailed comparisons with experimental data.

1.4. Bridge to Chapter 2: Introduction of the Five-Operator Functionally Complete Set

1.4.1. Position and Purpose

We have already emphasised that the dynamics of the universe can be described solely with the single fermion Ψ . However, for clarity it is preferable to modularise the operator content so that physical functions become visible. Chapter 2 therefore adopts the set
S 5 = D , Π n , V n , Φ , R ,
a five-operator functionally complete set. The aim is to establish the Functional-Completeness Proposition (5-Op)—that “five operators suffice to reconstruct the full functionality of Ψ ”—rather than to assert minimality or uniqueness. This subsection organises (i) the roles of the five operators, (ii) the proof roadmap of Chapter 2, and (iii) the links to subsequent chapters, thereby bridging inter-chapter logic.

1.4.2. Five Operators and Their Roles

At the beginning of Chapter 2 an elimination experiment shows that omitting any element of S 5 obscures specific functionalities. The correspondence is summarised in Table 1.

1.4.3. Claim of Functional Completeness

Although the theory closes when folded into the single Ψ , the introduction of S 5 dramatically enhances functional separation, readability, and computational convenience. The conclusion of the elimination experiment is that S 5 constitutes a usefully small basis, though not minimal, for decomposing the functions of Ψ into information-theoretic, dissipative, and geometric sectors.

1.4.4. Structure and Roadmap of Chapter 2

  • §2.1 Declaration Presents the Functional-Completeness Proposition (5-Op).
  • §2.2 Foundations Defines C * -algebras, CPTP maps, and fractal measures.
  • §2.3–2.7 Constructs each operator and verifies its assigned role.
  • §2.8 Proof of Functional Completeness Demonstrates algebraic closure and preservation of CPTP maps.
  • §2.9 Bridge Specifies where these operators are used in later chapters.

1.4.5. Links to Subsequent Chapters

  • Chapter 3 — With { D , Π n , V n } proves the Three-Form Equivalence Theorem (operator, variational, and field-equation forms).
  • Chapters 4–6 — Analyse information dissipation and measurement processes (thermalisation, quantum Zeno effect, etc.).
  • Chapters 7–10 — Derive Yukawa matrices and the mass hierarchy from the exponential rule of Π n and V n .
  • Chapters 11–13 — Use Φ and R to coherently treat GR reduction, the BH information problem, and cosmological parameters.

1.4.6. Summary

The five-operator functionally complete set decomposes the full behaviour of Ψ into the aspects of time evolution, projection, dissipation, geometry, and vacuum stability. Hereafter, this paper adopts S 5 as the standard set for explanation and calculation, reintegrating it into Ψ where necessary to streamline the discussion.

2. Five Operators and the Canonical Decomposition Theorem (Functional Completeness)

2.1. Statement of the Theorem and Proof Strategy

2.1.1. Introduction and Notational Conventions [1,2,3]

For the sake of visual clarity and computational convenience, the functions contained in the single fermion Ψ are operationally partitioned into the following five-operator set
D , Π n ( n = 1 , , 18 ) , V n = γ Π n , Φ , R , ( γ > 0 ) ,
denoted by S 5 . Here D — reversible generator, Π n — mutually orthogonal projection operators, V n — GKLS-type dissipative jump operators, Φ — scalar field with normalised four-gradient (to be specified in Eq. (3)), R — zero-area resonance kernel with exponential area convergence.
This subsection declares:
  • that S 5 provides a canonical decomposition (functional completeness) whose elements satisfy all functional requirements without redundancy;
  • the existence of a bijective map
    G : Φ ( D , Π n , V n , R )
    between the scalar Φ and the remaining operators (Φ Generating Map Theorem);
  • that omitting any element of S 5 breaks one of the functional requirements, making it the minimal practical basis that preserves all functions without loss.
A roadmap for the proofs is also provided.

2.1.2. Theorem 2.1 — Canonical Decomposition Theorem and Φ Generating Map Theorem [4,5]

Theorem 1
(Canonical Decomposition Theorem (Functional Completeness) and Φ Generating Map Theorem).
(i) 
On a Hilbert space H there exists a set of operators ( D , Π n , V n , R ) simultaneously satisfying the following conditions. Any two such sets are related by a unitary transformation Π n U Π n U ( U U ( H ) ) and a rescaling of γ:
(a)
Reversible unitary generator D — self-adjoint, [ D ] = 0 , locally Lorentz covariant.
(b)
Measurement basis  { Π n } Π n Π m = δ n m Π n , n = 1 18 Π n = I .
(c)
Dissipative jump operators  V n = γ Π n — generate a CPTP semigroup.
(d)
GR-reduction scalar Φ — normalised four-gradient a Φ a Φ = 1 .
(e)
BH information-retention kernel R — zero-area kernel with area-exponential convergence R A e λ A and information-preservation constraint [ R ρ ] = 0 .
(ii) 
If a scalar Φ satisfies
a Φ a Φ = 1 ,
then the map G : Φ ( D , Π n , V n , R ) is bijective. The inverse map G 1 is uniquely given by
Φ ( x ) = x g a b J a J b d s , J a : = ϵ a b c d Π n b Π n c Π n d Π n .
(iii) 
Removing any single element of S 5 results in the loss of at least one functional requirement—reversible unitarity, CPTP dissipation, measurement basis, GR reduction, or BH information-retention/vacuum stability. Hence S 5 is apractically irreducible basisthat preserves all functionality.

2.1.3. Overview of the Proof Strategy [6,7]

(S1) 
Uniqueness of Φ normalisation — Eq. (3) determines Φ up to an additive constant and an overall sign.
(S2) 
Construction of the generating map G — Starting from Φ , sequentially define
D : = i , · , Π n : = χ Ω n ( Φ ) , V n : = γ Π n , R : = lim A 0 A 1 K A [ Φ ] ,
and verify conditions (a)–(e) (§2.3–§2.7).
(S3) 
Elimination of redundant degrees of freedom — Show that conditions (a)–(e) fix all degrees of freedom except for unitary transformations and scale rescalings, which reduce to projector equivalence classes.
(S4) 
Construction of the inverse map G 1 — Prove that ( D , Π n , V n , R ) uniquely reconstruct Φ via the J a -current integral formula.

Conclusion

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2.2. Mathematical Preliminaries: C*-Algebras, CPTP Semigroups, and Tetrad Normalization

In this subsection we arrange the mathematical foundations necessary to construct the five-operator set S 5 = { D , Π n , V n , Φ , R } rigorously and to prove the Canonical Decomposition Theorem (Theorem 1). The topics covered are
1
C*-algebras and GNS representations,
2
Completely positive trace-preserving (CPTP) maps and the Kraus representation,
3
Quantum dynamical semigroups generated by GKLS operators,
4
Four-gradient–normalised scalars and tetrad construction.

2.2.1. Basics of C*-Algebras and GNS Representation [8,9,10]

Definition 1
(C*-Algebra). A norm-complete *-algebra ( A , · , * ) that satisfies the spectral condition A * A = A 2 is called a C*-algebra.
Lemma 1
(Uniqueness of the GNS Representation). For a positive linear functional ω : A C , the GNS triple π ω , H ω , | Ω ω constructed from ω is unique up to unitary equivalence.
Proof. 
Let N ω : = { A A ω ( A * A ) = 0 } . On the quotient A / N ω introduce the inner product [ A ] , [ B ] ω : = ω ( A * B ) . Completing this space yields H ω . The map π ω ( A ) [ B ] : = [ A B ] is a *-homomorphism, and the standard argument gives the claimed uniqueness.     □

2.2.2. Completely Positive Trace-Preserving Maps and the Kraus Representation [11,12,13,14]

Definition 2
(CPTP Map). For the finite-dimensional C*-algebra A = B ( H ) , a linear map E : A A is called completely positive and trace-preserving (CPTP) if, for every n N , E id n is positive and [ E ( A ) ] = [ A ] holds.
Theorem 2
(Kraus Representation Theorem). A linear map E is CPTP iff there exists a finite set { K α } A such that
E ( A ) = α K α A K α , α K α K α = 1 .
Proof. 
Diagonalise the Choi matrix C E : = i j | i j | E ( | i j | ) as C E = α | ϕ α ϕ α | . Then define K α : = α | ϕ α , which serve as Kraus operators. The converse follows from the Choi–Jamiołkowski isomorphism.     □

2.2.3. GKLS Generators and Quantum Dynamical Semigroups [15,16,17,18]

Theorem 3
(GKLS Generator). Let { T t } t 0 be a CPTP semigroup with continuous parameter t 0 . Its infinitesimal generator L : = d d t | t = 0 T t necessarily takes the form
L [ ρ ] = i [ H , ρ ] + α L α ρ L α 1 2 { L α L α , ρ } ,
and conversely, any such H = H and set { L α } uniquely determine the semigroup.
Proof. 
Follow the standard proof combining Lindblad’s matrix-element calculation with the diagonalisation method of Gorini–Kossakowski–Sudarshan–Lindblad.     □

2.2.4. Four-Gradient–Normalised Scalars and Tetrad Construction

Definition 3
(Four-Gradient–Normalised Scalar). A scalar field Φ satisfying
a Φ a Φ = 1
is called a four-gradient–normalised scalar. Defining the unit timelike vector u a : = a Φ and choosing an orthonormal spatial triad { e i a } i = 1 3 orthogonal to u a , one obtains a uniquely determined tetrad e μ a = ( u a , e i a ) .
Lemma 2
(Uniqueness of the Tetrad). Under the above normalisation, e μ a is unique up to local SO ( 3 ) rotations.
Proof. 
Since u a fixes the timelike direction, the remaining freedom is precisely the three-dimensional rotation in the spatial subspace.     □

2.2.5. Conclusion and Bridge to Subsequent Sections

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2.3. Normalization of the Master Scalar Φ and the Generating Map

2.3.1. Normalization Condition and Phase Degrees of Freedom [19,20]

The master scalar  Φ : M R , which lies at the heart of the single-fermion UEE, satisfies on the space–time manifold ( M , g a b )
a Φ a Φ = 1
This condition guarantees that
1
Φ is a Cauchy time function;
2
its level sets possess a unit normal u a : = a Φ ;
3
Φ is unique up to the phase freedoms Φ Φ + c and Φ Φ .
Lemma 3
(Uniqueness of Φ ). A pure, integrable scalar field Φ satisfying (3) is unique except for a constant shift and an overall sign.
Proof. 
Set u a : = a Φ ; then u a u a = 1 and—by the Frobenius condition— u [ a b u c ] = 0 . Hence Φ coincides with the proper time τ along u a , leaving only the freedoms τ τ + c and τ τ .     □

2.3.2. Mapping from Φ to the Tetrad [21,22]

Definition 4
( Φ -Induced Tetrad). Define e a 0 : = u a = a Φ and, with h a b : = δ b a u a u b , set
e a ı ^ : = h a b L u ı ^ 1 u b , ı ^ = 1 , 2 , 3 .
Gram–Schmidt orthonormalisation then yields the tetrad { e a μ } μ = 0 3 .
Lemma 4
( Φ –Tetrad Correspondence). Under condition (3), Φ and the tetrad e a μ are in one-to-one correspondence.
Proof. 
The relation e a 0 = u a = a Φ follows immediately. The spatial triad e a ı ^ is uniquely fixed as an orthonormal basis of h a b ; conversely, line integration of u a reconstructs Φ ( x ) = γ u a ξ a .     □

2.3.3. Construction of the Φ Generating Map [23,24]

From the master scalar Φ we define the generating map  G that constructs the operator set S 5 = { D , Π n , V n , R } (excluding Φ itself):
D : = i γ μ e μ a a ,
Π n : = 1 2 1 + σ n u a Γ a λ n , n = 1 , , 18 ,
V n : = γ Π n ,
R : = lim A 0 1 A exp A L u
Here γ μ are the Dirac matrices, σ n = ± 1 encode the exponential rule, and λ n are real constants uniquely fixed by the Yukawa hierarchy indices { 0 , 1 , 3 , 5 , } .

2.3.4. Invertibility of the Generating Map [25]

Theorem 4
( Φ Generating Map Theorem). The map G : Φ ( D , Π n , V n , R ) is bijective. Its inverse is uniquely given by
Φ ( x ) = x 0 x g a b J a J b ξ , J a : = ϵ a b c d Π n b Π n c Π n d Π n
Proof. 
Injectivity: If Φ Φ then u a u a , hence the tetrads differ and at least D differs, so G ( Φ ) G ( Φ ) .
Surjectivity: Suppose a set ( D , Π n , V n , R ) satisfies (4)–(7). Then u a : = e a 0 is a closed one-form, so there exists Φ with u a = a Φ , uniquely determined by (8).     □

2.3.5. Conclusion

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2.4. Canonical Form of the Reversible Generator D = G D [ Φ ]

2.4.1. Definition and Assumptions [26]

Definition 5
( Φ -Induced Dirac Operator). For the tetrad { e a } μ induced by the four-gradient–normalised scalar Φ (see Lemma 2), define the reversible generator (Φ-induced Dirac operator) by
D : = i γ μ e μ a a + 1 4 ω a b c γ [ b γ c ]
In this subsection we show that (9) is the canonical form that simultaneously satisfies
1
self-adjointness,
2
local Lorentz covariance,
3
the fixed point β D = 0 .

2.4.2. General Candidate and the Self-Adjointness Condition [27]

A general first-order spinor operator can be written as
D ˜ = i γ μ e μ a a + 1 4 ω a γ [ b b c γ c ] + A a + i B a γ 5 + M + i M 5 γ 5 ,
where A a , B a are vector fields and M , M 5 are scalar fields.
Lemma 5
(Self-Adjointness Criterion). The operator D ˜ is self-adjoint with respect to the Dirac inner product ( ψ , φ ) : = ψ ¯ φ g d 4 x ( D ˜ = D ˜ ) iff
A a = 0 , B a = 0 , M = 0 , M 5 = 0 .
Proof. 
Take the Hermitian adjoint using ( γ μ ) = γ 0 γ μ γ 0 . Comparing the coefficients of D ˜ D ˜ , any of the four fields left non-zero would yield an anti-Hermitian contribution, which is forbidden.     □

2.4.3. Requirement of Local Lorentz Covariance [19]

Dirac spinors transform under the double-cover representation of SL ( 2 , C ) . For D ˜ to be covariant, the extra terms in (10)— A a , B a , M , M 5 —must be Lorentz scalars; by Lemma 5 they are all zero, reducing the operator to (9).
Lemma 6
(Torsion-Free Spin Connection). The spin connection ω a b c of the tetrad induced by Φ coincides with the Levi-Civita connection and satisfies torsion-free condition T a = [ b c ] 0 .
Proof. 
From a Φ a Φ = 1 and the Frobenius condition u [ a b u c ] = 0 with u a : = a Φ , the torsion three-form in Cartan’s structure equation vanishes.     □

2.4.4. β D = 0 Fixed Point [28,29]

For the reversible generator the effective action S D = ψ ¯ D ψ g d 4 x has 1-loop β-function
β D = N f N ˜ f 24 π 2 M 3 ,
where N f is the number of fermionic degrees of freedom and N ˜ f : = 16 Tr ( B a B a ) . With M = B a = 0 from Lemma 5 we obtain
β D = 0 .

2.4.5. Canonical-Form Theorem

Theorem 5
(Canonical Form of the Reversible Generator). Given the tetrad induced by Φ, any first-order Dirac operator that simultaneously satisfies
1 
self-adjointness,
2 
local Lorentz covariance,
3 
the fixed point β D = 0 ,
is equivalent to (9) up to unitary projector equivalence D U D U with U U ( H ) .
Proof. 
Starting from the general form (10) and applying Lemmas 5 and 6 in succession, all surplus parameters are removed except for a phase and projector equivalence. These do not affect the physics, leaving (9) as the unique canonical form.     □

2.4.6. Conclusion

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2.5. Pointer Projector Family Π n = G Π [ Φ ] and Minimality

2.5.1. Definition of the Projector Family and the Internal Hilbert Space [30,31]

Definition 6
(Internal Hilbert Space). The internal degrees of freedom of Standard-Model fermions are the direct product of colour ( dim = 3 ) , weak isospin ( dim = 2 ) , and generation ( dim = 3 ) :
H int : = C color 3 C weak 2 C generation 3 C 18 .
We choose an orthonormal basis | c i | w j | g k ( i = 1 : 3 , j = 1 : 2 , k = 1 : 3 ) .
Definition 7
(Pointer Projector Operators). For the triple index n = ( i , j , k ) define
Π i j k : = | c i w j g k c i w j g k | , n ( i , j , k ) , n = 1 , , 18 .
Collectively we denote the 18 projectors by { Π n } n = 1 18 .

2.5.2. Verification of Orthogonality and Completeness [32,33]

Lemma 7
(Orthogonality). For any n m one has Π n Π m = 0 , and Π n 2 = Π n .
Proof. 
Equation (11) defines one-dimensional projectors, so Π n 2 = Π n . Because the basis vectors are orthogonal, the product vanishes for n m .     □
Lemma 8
(Completeness). n = 1 18 Π n = 1 int .
Proof. 
The 18 basis vectors form an orthonormal system spanning C 18 ; hence the projectors give a complete resolution of the identity.     □

2.5.3. Minimality Theorem [34]

Theorem 6
(Minimality of the Pointer Projector Family). Any projector family satisfying simultaneously
1 
orthogonality: Π n Π m = δ n m Π n ,
2 
completeness: n Π n = 1 int ,
3 
each image of Π n is one-dimensional,
requires at least 18 projectors. The set { Π i j k } defined in (11) is thereforeminimalin both number and structure.
Proof. 
Since dim H int = 18 , a complete resolution by one-dimensional projectors necessitates at least 18 of them. Lemmas 7 and 8 show that (11) meets conditions (1) and (2); with fewer projectors completeness would be lost.     □

2.5.4. Generating Map G Π from Φ [30]

On each level surface Σ τ of the master scalar Φ we employ the reference tetrad e a ı ^ and define an index map Ξ int : Σ τ { 1 , , 18 } (unique from the topological structure and group representations). We set
G Π [ Φ ] : Π n ( x ) = χ { Ξ int ( x ) = n } | c i w j g k c i w j g k | , n = 1 , , 18 .
Thus the family { Π n } is generated from Φ bijectively.

2.5.5. Uniqueness up to Projector Equivalence

Lemma 9
(Uniqueness under Projector Equivalence). With Φ fixed, the projector family { Π n } is unique up to unitary conjugation U Π n U = Π n ( U U ( H int ) ).
Proof. 
Unitary transformations preserving conditions (1)–(3) are restricted to diagonal unitaries that attach phases to each basis vector. Physical observables are phase-independent, so these families are considered equivalent.     □

2.5.6. Conclusion

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2.6. Jump Operators V n = γ Π n and Canonical Dissipation

2.6.1. Definition of the Jump Operators [15,16]

Given the pointer projector family { Π n } n = 1 18 (Lemma 8) and a positive dissipation rate γ > 0 , define
V n : = γ Π n , n = 1 , , 18 .
We shall show that (12) constitutes the canonical form of dissipation, because it
1
guarantees complete positivity and trace preservation when constructing the GKLS generator, and
2
minimises the Choi–Kraus rank to 18.

2.6.2. Rank Analysis of the GKLS Generator [12,35]

Together with the reversible generator D, the Lindblad–GKS generator reads
L [ ρ ] = n = 1 18 V n ρ V n 1 2 { V n V n , ρ } = γ n Π n ρ Π n 1 2 { Π n , ρ } .
Because of the projector property Π n 2 = Π n and completeness n Π n = 1 int , (13) generates a CPTP semigroup (Theorem 3).
Lemma 10
(Rank Minimisation). When Π n are one-dimensional projectors, the Choi–Kraus rank of the Lindblad generator (13) is
R min = 18 .
Proof. 
The Choi matrix C L : = i j | i j | L ( | i j | ) breaks into 18 one-dimensional blocks owing to the orthogonality of { Π n } , giving C L = 18 . A rank smaller than 18 would imply that at least two Π n have merged, breaking completeness, a contradiction.     □

2.6.3. Redundancy of Phase Freedom [36]

Multiplying each Π n by a phase preserves the projector property:
V n : = e i θ n γ Π n .
Substituting V n into (13) cancels all phases, yielding L = L . Thus physical observables do not depend on { θ n } ; the phases amount to projector-equivalent freedom.

2.6.4. Canonical Dissipation Theorem

Theorem 7
(Canonical Form of Dissipation). The jump-operator set that simultaneously satisfies
1 
completeness n V n V n = γ 1 int ,
2 
minimal rank C L = 18 ,
is equivalent to (12) up to phase freedom V n e i θ n V n .
Sketch. 
Condition (1) implies V n = γ U n Π n with partial unitaries U n . One finds Π n U n Π n = e i θ n Π n ; condition (2) forbids any contraction other than phase factors, fixing the canonical form.     □

2.6.5. Universality of the Decoherence Time [17]

Diagonalising (13), the matrix elements decay as ρ m n ( t ) = ρ m n ( 0 ) exp [ γ t / 2 ] for m n . The decoherence time is therefore
τ dec = γ 1 ,
a universal constant independent of the pointer basis.

2.6.6. Conclusion

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2.7. Zero-Area Resonance Kernel R = G R [ Φ ]

Note) For the derivation and justification of the zero-area resonance kernel R, see the existing study “Deriving the Area-Term Cancelling Operator and Axiomatizing Information-Flux Dynamics’’ (DOI: 10.5281/zenodo.15701805) [465].

2.7.1. Definition and Four Requirements

Definition 8
(Zero-Area Resonance Kernel). On the level surface Σ τ of the master scalar Φ, let u a : = a Φ denote the unit normal vector. Using the Lie flow exp ( s L u ) along u a , define
R : = lim ε 0 + 1 ε exp ε L u
The four requirements that (14) must satisfy are:
i
Self-adjointness R = R ;
ii
Zero-area scaling R A e λ A ( A 0 ) ;
iii
Information preservation [ R ρ ] = 0 ρ ;
iv
Vacuum-energy stabilisation  0 | R | 0 = 0 | T μ | 0 μ .1

2.7.2. Fredholm Construction and Zero-Area Limit [37,38]

Lemma 11
(Fredholm-kernel representation). exp [ ε L u ] is a compact operator and possesses the Fredholm kernel K ε ( x , y ) = δ Φ ( x ) Φ ( y ) ε .
Lemma 12
(Zero-area limit). The zero-area resonance kernel R = lim ε 0 + ε 1 exp [ ε L u ] has matrix element x | R | y = δ Φ ( x ) Φ ( y ) , and satisfies the norm estimate R ε e λ ε .
Proof sketch. 
Applying a Taylor expansion to the Fredholm-kernel representation, the derivative of the Dirac δ appears in the first-order term. The Hilbert–Schmidt norm estimate yields the above inequality.     □

2.7.3. Self-Adjointness, Information Preservation, and Vacuum Stabilisation

Lemma 13
(Self-adjointness). L u generates a geodesic flow with zero divergence, and exp [ ε L u ] is unitary. Hence R = R .
Lemma 14
(Information preservation). For any density operator ρ, [ R ρ ] = 0 .
Idea. 
Because the derivative of the Dirac δ balances signs on the diagonal, the trace vanishes.     □
Lemma 15
(Vacuum-energy stabilisation). Using the Hadamard expansion near the coincidence limit, 0 | R | 0 = 0 | T μ | 0 μ .
Sketch. 
The δ structure cancels the constant term of the zero-point energy.     □

2.7.4. Uniqueness Theorem

Theorem 8
(Canonical form of the zero-area resonance kernel). Any kernel R satisfying simultaneously the requirements (i)–(iv) is, up to a phase degree of freedom R e i θ R e i θ , uniquely given by the definition (14).
Outline 
The δ structure is fixed by zero-area scaling, the coefficient becomes real by self-adjointness, and normalisation is determined by information preservation and vacuum stabilisation; only (14) remains.     □

2.7.5. Invertibility of the Generation Map

Because R is defined as the differential limit of L u , u a = a Φ can be reconstructed uniquely. Integrating u a = a Φ also reconstructs Φ uniquely (Theorem 4). Therefore the generation map G R : Φ R is invertible.

2.7.6. Conclusion

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2.8. Functional Independence of the Five Operators and the Functional Completeness Set

2.8.1. Functional Matrix of the Five Operators [2]

Table 2. Correspondence between the five operators and basic functional requirements
Table 2. Correspondence between the five operators and basic functional requirements
Requirement D Π n V n Φ R
Reversible unitarity
CPTP dissipation
Measurement basis
GR reduction
BH information retention + vacuum stability
Correspondence between the five operators and basic functional requirements

2.8.2. Independence Lemma [34,35]

Lemma 16
(Functional Independence). In Table 2, each operator contributesuniquelyto at least one requirement and cannot be replaced by the others.
Sketch. 
Example: BH information retention + vacuum stability requires the zero-area kernel R with exponential area convergence (Theorem 8); no other operator possesses that property. Similarly, GR reduction uniquely needs the Φ -tetrad, the measurement basis requires one-dimensional pointer projectors, etc.     □

2.8.3. Verification by Removal Experiments

(a) 
D 0 The unitary limit cannot be reproduced (Theorem 5).
(b) 
Π n Π ˜ n The Born rule is violated and measurement probabilities become undefined.
(c) 
V n 0 Decoherence time τ dec , contradicting experiments.
(d) 
Φ externally fixed Tetrad construction and GR reduction become impossible (Lemma 2).
(e) 
R 0 Information is lost in BH evaporation and a cosmological constant shift δ ρ vac 0 arises.
Each removal breaks at least one requirement, destroying theoretical consistency.

2.8.4. Functional Completeness Theorem

Theorem 9
(Five-Operator Functional Completeness). The operator set S 5 = { D , Π n , V n , Φ , R } is a functionally complete basis that satisfies every requirement of the single-fermion UEE (reversible unitarity / CPTP dissipation / measurement basis / GR reduction / BH information retention + vacuum stability), because
1 
it possesses functional independence as per Lemma 16, and
2 
the necessity of each element is demonstrated by removal experiments (a)–(e).
We do not claim absolute minimality: all functions could, in principle, be compressed into the single operator Ψ, but S 5 represents thesmallest useful decompositionfor readability and computational convenience.
Proof. 
Any proper subset fails at least one requirement (removal experiments). Adding further operators introduces no new requirement columns in Table 2, so they are redundant. Hence S 5 is functionally complete as an operational decomposition.     □

2.8.5. Conclusion

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2.9. Summary of Chapter 2 and Connection to the Next Chapter

2.9.1. Key Points Established in This Chapter

I 
Unique determination of the master scalar Φ We proved that the four-gradient normalization a Φ a Φ = 1 fixes Φ as a time function, unique up to phase freedoms (constant shift and overall sign).
II 
Construction of the five-operator functionally complete set S 5 Via a bijective map from Φ we generated D , Π n , V n = γ Π n , R , showing that they cover—without redundancy—the five requirements: reversible unitarity, dissipation, measurement basis, GR reduction, and BH information retention / vacuum stability.
III 
Establishment of canonical (projector-equivalent) uniqueness We showed that each operator, including the standard first-order Dirac form D = i γ μ e μ a ( a + 1 4 ω a γ [ b b c γ c ] ) , possesses no redundant degrees of freedom other than phase rotations or unitary conjugation.
IV 
Independence check via the functional matrixTable 2 visualises the unique contribution of each operator to the five requirements; removal experiments confirmed that the basis is “complete but not minimal’’ in a practical sense.
V 
Establishing the bijection Φ S 5 By exhibiting the generating map G and its inverse G 1 , we demonstrated that all theoretical information can be described equivalently either by a single scalar or by five operators.

2.9.2. Logical Bridge to Chapter 3—Preparation for the Three-Form Equivalence Theorem

  • Operator-form foundation Chapter 3 opens with the operator form UEE op   ρ ˙ = i [ D , ρ ] + L [ ρ ] , constructed directly from the D and jump generator L [ ρ ] = n ( V n ρ V n 1 2 { V n V n , ρ } ) fixed in this chapter, so conservation laws hold immediately at the operator level.
  • Mapping to the variational form Section 3.3 uses the path-integral variational principle to prove UEE op UEE var ; the tetrad expansion and spin connection ω a b c required there directly employ the Φ-tetrad results of this chapter.
  • Mapping to the field-equation form Applying the Euler–Lagrange variation to the variational form yields the field-equation form UEE fld . The zero-area resonance kernel R provides the curvature-term coefficient reproducing the Einstein–Hilbert action; details appear in §3.4.
  • Introduction of the dissipation scale The decoherence time defined here, τ dec = γ 1 , enters directly into entropy production and conserved-quantity analyses (Spohn inequality) at the end of Chapter 3.

2.9.3. Guidelines for the Reader

  • Choice of representation: From here on we switch freely between the Φ description and the S 5 description according to computational convenience— S 5 for gauge-theoretic calculations, the Φ-tetrad for geometric arguments, and so on.
  • Proof roadmap: Chapter 3 proves the complete equivalence of the three forms (operator, variational, field-equation), establishing the representation invariance of the UEE. Proofs proceed Lemma → Theorem, referencing the lemma and theorem numbers introduced in this chapter where necessary.

2.9.4. Facts Confirmed Here

The five-operator functionally complete set is not claimed to be absolutely minimal, yet it satisfies functional independence and completeness while maximising computational clarity—hence adopted as the practical minimal basis. On this footing, the next chapter rigorously develops the three-form equivalence, conservation laws, and the variational principle of the UEE.

3. Unified Evolution Equation and Three-Form Equivalence

3.1. Statement of the Theorem and Proof Strategy

3.1.1. Definition of the Three Forms [15,16,39,40,41]

( i ) Operator form UEE op : ρ ˙ = i [ D , ρ ] + L diss [ ρ ] + R [ ρ ] ,
( ii ) Variational form UEE var : δ S UEE [ ψ , ψ ¯ , Φ ] = 0 ,
( iii ) Field - equation form UEE fld : G a b = 8 π T a b ( Φ , ψ , ψ ¯ ) + T a b diss , i ψ + M eff ψ = 0 , a ( a Φ ) = J res ,
where T a b diss and J res are dissipative source terms arising from the jump operators V n and the zero-area kernel R, respectively.

3.1.2. Statement of the Equivalence Theorem [19,42]

Theorem 10
(Three-Form Equivalence Theorem). For the master scalar Φ and the five-operator functionally complete set D , Π n , V n , Φ , R (Chapter 2), the operator form (15), the variational form (16), and the field-equation form (17) are
UEE op UEE var UEE fld
mutually and reversibly equivalent.

3.1.3. Roadmap of the Proof Strategy [12,43,44,45]

(S1) 
Operator form ⇒ Variational form Using the GNS representation we map operator expectation values ρ O to path-integral expressions and show, line by line, that they coincide with the Green functions of the variational action S UEE (§3.5).
(S2) 
Variational form ⇒ Field-equation form Including the Φ-tetrad and the zero-area kernel R among the variational variables, we prove that the Euler–Lagrange equations are in one-to-one correspondence with the set { G a b , ψ , Φ } (§3.6).
(S3) 
Field-equation form ⇒ Operator form Via the Wigner–Weyl transform we reconstruct operator commutators from the field-theoretic Poisson structure, recovering (15) with dissipative and zero-area terms included (§3.7).
(S4) 
Uniqueness of solutions and consistency of conserved quantities Local solutions are obtained by a Banach fixed-point argument and extended globally using the zero-area kernel. We verify that energy flux and entropy production are identical across the three forms (§3.8–3.9).

3.1.4. Conclusion

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3.2. Derivation of the Operator Form UEE op

3.2.1. Recap of the Five Operators and Basic Structure [46,47]

Using the five-operator functionally complete set (§2.8)
D , Π n , V n = γ Π n , Φ , R ,
we express the time evolution of the density operator ρ ( t ) as
ρ ˙ = i [ D , ρ ] + L diss [ ρ ] + R [ ρ ]

3.2.2. Derivation of the Dissipator [15,16,48]

From the Kraus representation theorem (Theorem 2) and the jump operators V n = γ Π n we obtain
L diss [ ρ ] = n = 1 18 V n ρ V n 1 2 { V n V n , ρ } = γ n Π n ρ Π n 1 2 { Π n , ρ } .
Lemma 17
(CPTP Property). The generator L diss is completely positive and trace-preserving; hence exp ( t L diss ) forms a CPTP semigroup.
Proof. 
Orthogonality and completeness of the projector family { Π n } (Lemmas 7, 8) give n V n V n = γ n Π n = γ 1 , so (3.2.2) is of Lindblad form.     □

3.2.3. Action Form of the Zero-Area Kernel R [37,49]

Acting definition (14) on the density operator yields
R [ ρ ] : = lim ε 0 + 1 ε e ε L u ρ ρ = L u ρ ,
where L u ρ : = u a a ρ . By Lemma 13 R is self-adjoint, and Lemma 14 gives [ R [ ρ ] ] = 0 .

3.2.4. Final Form of the Operator UEE [17]

Substituting (3.2.2) and (3.2.3) into (3.2.1) we obtain
ρ ˙ = i [ D , ρ ] + γ n = 1 18 Π n ρ Π n 1 2 { Π n , ρ } L u ρ
Theorem 11
(Functional Completeness of the Operator Form UEE op ). Equation (3.2.4) simultaneously contains
1 
the unitary part generated by the self-adjoint D,
2 
the Lindblad dissipative part L diss ,
3 
the information-retention part supplied by the zero-area kernel R,
and is afunctionally complete evolution equationthat preserves the trace and complete positivity.
Proof. (i) Trace preservation follows immediately from the CPTP property of exp ( t L diss ) and [ R [ ρ ] ] = 0 . (ii) Complete positivity is guaranteed by the Lindblad form of L diss and the commutator-type, self-adjoint structure of R, satisfying the Gorini–Kossakowski conditions. By the functional completeness theorem of Chapter 2 (Theorem 9), any additional term would be redundant, while omission of any term would diminish functionality; hence (3.2.4) is the operationally unique form.     □

3.2.5. Conclusion

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3.3. Derivation of the Variational Form UEE var

3.3.1. Field variables and design guidelines for the action [42,50]

To transplant the five-operator complete set into field variables we take the basic variational variables
ψ ( x ) , ψ ¯ ( x ) , Φ ( x ) , ( x M ) ,
where ψ is the single-fermion Dirac spinor, ψ ¯ : = ψ γ 0 , and Φ is the master scalar normalised in Chapter 2.

3.3.2. Construction of the action [24,51]

(1) Reversible part

With the Φ-induced tetrad e a ( Φ ) μ and spin connection ω a b c ,
L rev = ψ ¯ i γ μ e μ a ( a + 1 4 ω a b c γ [ b γ c ] ) ψ .

(2) Dissipative part

With the pointer projectors Π n and jumps V n = γ Π n interpreted as projector fields Π n ( ψ , ψ ¯ ) ,
L diss = γ n = 1 18 ψ ¯ Π n ψ 1 2 ψ ¯ { Π n , Π n } ψ .

(3) Resonance part

Linear (flow) term corresponding to the zero-area kernel R:
L R = ψ ¯ L u ψ , u a : = a Φ .

(4) Total action

S UEE : = M d 4 x g L rev + L diss + L R

3.3.3. Variation and Euler–Lagrange equations [52]

Lemma 18
(Euler–Lagrange equations). The variation δ S UEE = 0 of the action (18) yields for the spinor fields
i [ D , ρ ] + γ n Π n ρ Π n 1 2 { Π n , ρ } L u ρ = 0 ,
where ρ : = | ψ ψ | .

Proof

Separate the δ ψ ¯ and δ ψ terms: the reversible part reproduces the Dirac equation; the dissipative part matches the GKLS form via the Kraus expansion; the L u term produces the flow derivative. Collecting terms reproduces the operator form (3.2.4). □

3.3.4. Derivation of conserved quantities [53]

Under a Φ-time translation δ t = ϵ the Noether charge
Q E : = Σ τ d 3 x h ψ ¯ γ 0 ψ
is conserved: Q ˙ E = 0 . The dissipator obeys [ L diss [ ρ ] ] = 0 , while L u is a Lie transport that leaves the total amount unchanged.

3.3.5. Fixing the variational form UEE var [54]

Theorem 12
(Variational form). The action (18) is (i) locally Lorentz-covariant, (ii) gauge-covariant, (iii) invariant under Φ-flow, and the condition δ S UEE = 0 reproduces the operator form UEE of Lemma 18.

Proof

(i)(ii) follow from the tetrad–spinor construction and the gauge covariance of the projectors; (iii) from the covariance of L u as a Lie derivative. The Euler–Lagrange derivation has already been given. □

3.3.6. Conclusion

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3.4. Derivation of the Field-Equation Form UEE fld

3.4.1. Φ -tetrad and rearrangement of the effective action [55,56]

Using the four-gradient normalisation a Φ a Φ = 1 and Lemma 2 (Chapter 2) we construct the tetrad e a ( Φ ) μ . Embedding the five-operator complete set { D , Π n , V n , Φ , R } into the covariant action principle and performing the ( t , x i ) space-time split yields
S UEE = 1 16 π g R S EH [ g ( e ) ] + g ψ ¯ D ψ S SM + γ g ψ ¯ n Π n 1 2 ψ S diss = g ψ ¯ L u ψ S R .
Here u a : = a Φ ; S EH is the Einstein–Hilbert action; S SM is the reversible single-spinor Standard-Model part built with the Dirac operator D; S diss originates from the Lindblad dissipation via the jump operators V n ; S R is the action form of the zero-area resonance kernel.

3.4.2. Metric variation: gravitational field equation [19,40]

(1) Metric variation.

Writing g a b = e a e b μ η μ ν ν and setting δ S UEE / δ g a b = 0 we obtain
G a b = 8 π T a b SM + T a b diss + T a b R ,
with
T a b diss : = 2 g δ S diss δ g a b , T a b R : = 2 g δ S R δ g a b .

(2) Contribution of the zero-area term.

Variation of S R = g ψ ¯ L u ψ gives T a b R = ( a ( ψ ¯ γ b ) ψ ) g a b c J c with J c : = ψ ¯ γ c ψ . Because of the exponential area convergence (Lemma 12) we have | T a b R | Area e λ Area 0 ; globally only the BH-island correction survives.

3.4.3. Spinor variation: fermionic equation [57]

From δ S UEE / δ ψ ¯ = 0 we obtain
i γ μ e μ a ( a + 1 4 ω a γ [ b b c γ c ] ) ψ + γ n Π n 1 2 ψ L u ψ = 0 .
The first term is the reversible Dirac part, the second implements dissipative diagonalisation, the third is the zero-area flow term.

3.4.4. Variation of Φ : scalar equation [58]

Variation δ S UEE / δ Φ = 0 gives
a a Φ = J res : = 1 g δ S diss δ Φ .
The term γ ψ ¯ Π n ψ in S diss acts as the scalar source J res , linking to the exponential Yukawa law and fractal dissipation rate (see later chapters).

3.4.5. Collecting the field-equation form [42]

G a b = 8 π T a b SM + T a b diss + T a b R , i ψ + γ n Π n 1 2 ψ L u ψ = 0 , a a Φ = J res .
Theorem 13
(Functional completeness of the field-equation form). The system (3.4.5) determines, without free parameters, the (i) gravitational, (ii) matter, and (iii) scalar sectors of the single-fermion UEE, and is reversibly equivalent to both the variational form (16) and the operator form (3.2.4).
Sketch. 
The equations (3.4.5) are the Euler–Lagrange equations derived from S UEE ; applying the Wigner–Weyl transform maps the bilinear spinor terms into operator commutators, recovering the operator form. Conversely, the Weyl symbol expansion reconstructs g a b , ψ , Φ from the operator form.     □

3.4.6. Conclusion

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3.5. Proof of Equivalence UEE op UEE var

3.5.1. Definition of the generating functional [59,60]

Formally solving the operator form UEE (3.2.4) with the time-ordered exponential gives ρ ( t ) = G ( t ) ρ 0 where G ( t ) : = T exp 0 t L ( τ ) d τ . Introducing external sources η , η ¯ , define
Z op [ η , η ¯ ] : = G ( t ) T exp η ¯ ψ + ψ ¯ η d 4 x .

3.5.2. Lemma 1: GNS representation and path-integration [46,61]

Lemma 19
(GNS path integration). Any CPTP semigroup G ( t ) admits a GNS embedding on a Hilbert–Schmidt space, G ( t ) ρ = α K α ( t ) ρ K α ( t ) , and yields the functional representation
Z op [ η , η ¯ ] = D ψ D ψ ¯ exp i S eff [ ψ , ψ ¯ ] + i ( η ¯ ψ + ψ ¯ η ) .

Proof

Via the Choi–Jamiołkowski isomorphism the Kraus operators K α are obtained; inserting the fermionic coherent-state resolution of unity 1 = d ψ ¯ d ψ | ψ ψ | e ψ ¯ ψ and applying a Trotter decomposition followed by the continuum limit produces a Grassmann path integral. □

3.5.3. Lemma 2: Stratonovich transformation of the dissipator [62,63]

Lemma 20
(GKLS → quasi-classical field). Because the Kraus operators V n = γ Π n are rank-1, introducing Hubbard–Stratonovich variables ξ n ( x ) of Kullback–Leibler type gives
exp L diss = ^ D ξ n exp ψ ¯ Π n ξ n + ξ ¯ n Π n ψ i γ ξ ¯ n ξ n ,
reproducing the effective Lagrangian L diss (eq. (3.3.2)).

Proof

A rank-1 GKLS kernel can be decomposed via Gaussian completion of the square ([17], Eq. 3.77). Collecting terms yields linear couplings to the fermionic sources. □

3.5.4. Lemma 3: Functional reduction of the zero-area flow term [12]

Lemma 21
(Path-weight of the Lie flow L u ). The term L u ρ contributes linearly as ψ ¯ L u ψ in the coherent-path action.

Proof

Expanding the flow map e ε L u via the Trotter factorisation and taking the first-order limit adds the Lie-derivative density to the Lagrangian. □

3.5.5. Equivalence lemma [5]

Lemma 22
(Operator form ⇒ Variational form). Through Lemmas 19–21 the generating functional (3.5.1) becomes
Z op [ η , η ¯ ] = D ψ D ψ ¯ exp i S UEE + i ( η ¯ ψ + ψ ¯ η ) ,
where S UEE is precisely the variational action (18). Therefore the operator form (3.2.4) implies the variational condition δ S UEE = 0 .

Proof

Lemma 19 converts the framework to a path integral; Lemmas 20 and 21 absorb the dissipative and zero-area corrections into the effective action. The resulting action coincides with S UEE of §3.3, establishing invertible correspondence of all Green functions. □

3.5.6. Conclusion

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3.6. Proof of Equivalence UEE var UEE fld

3.6.1. Premise and Aim of the Variational Form [50]

Starting from the action obtained in the previous subsection
S UEE e a ( Φ ) μ , ψ , ψ ¯ , Φ , δ S UEE = 0 ,
our goal is to derive the set of coupled field equations (3.4.5) for the metric g a b , the fermion ψ , and the scalar Φ .

3.6.2. Lemma 1: Tetrad Variation and Recovery of Einstein–Hilbert Dynamics [51,64]

Lemma 23
( Φ -tetrad variation formula). With e a = μ e a ( Φ ) μ and δ e a = μ ( δ Φ ) b e a μ u b we have
δ g R = g G a b δ g a b + a Θ a ,
where Θ a is a boundary term.

Proof

Expand the Palatini variation via the chain rule, using the tetrad relation g a b = e a e b μ η μ ν ν . □

3.6.3. Lemma 2: Stress Tensor of the Dissipative Functional [48]

Lemma 24
(Dissipative stress T a b diss ). Varying S diss with respect to g a b gives
T a b diss = γ n Π n e a ψ ¯ μ γ μ e b ψ ν γ ν + ,
proportional to the first moment; it obeys a T a b diss = 0 .

Proof

Compute δ L diss / δ g a b via δ e a μ ; cross-terms vanish by pointer orthogonality. □

3.6.4. Lemma 3: Tracer of the Zero-Area Term [37]

Lemma 25
(Zero-area flow and stress term). The variation of S R with respect to g a b produces T a b R which is locally bounded as O ( Area e λ Area ) and whose back-reaction is confined to BH-island regions.

Proof

Insert the norm estimate from Lemma 12 into the stress-tensor definition. □

3.6.5. Proof of the Equivalence Theorem [65]

Lemma 26
(Variational form ⇒ Field-equation form). The Euler–Lagrange equations of S UEE coincide with the coupled field equations (3.6.5).

Proof

(i) Gravitational sector: Employ Lemma 23 for δ ( g R ) , add Lemmas 24 and 25, and recover Einstein’s equation (11.5.4).
(ii) Spinor sector: Setting δ S / δ ψ ¯ = 0 gives the Dirac equation (3.4.3) (see Lemma 18).
(iii) Scalar sector: δ S / δ Φ = 0 leads to the scalar equation (3.4.4).
Together these yield (3.4.5), establishing the reversible map from the variational to the field-equation form. □

3.6.6. Conclusion

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3.7. Bidirectional Invertibility: Operator Form ⇔ Field-Equation Form

3.7.1. Preparations for the Wigner–Weyl Transform [44,45,66]

On the space-time phase space Γ : = T * M × Z 18 , which includes the finite internal space C 18 , define
W : O ^ O W ( x , p , n ) : = d 4 y e i p · y x y 2 | O ^ | x + y 2 n .
Its inverse is given by Weyl quantisation O ^ = W 1 [ O W ] .

3.7.2. Lemma 1: Reversible Generator and Poisson Structure [67]

Lemma 27
(Dirac commutator → Poisson extension). For the reversible generator D one has
W i [ D , A ^ ] = { H op , A W } Moyal , H op : = W [ D ] .
In the expansion of the Moyal bracket the limit 1 yields the generalised Poisson bracket.

Proof

Using the Kontsevich star product A B = A exp [ i 2 Λ ] B , the leading regular term reproduces the Poisson bracket. Setting = 1 completes the correspondence. □

3.7.3. Lemma 2: Weyl Symbol of the Dissipative Kernel [68]

Lemma 28
(GKLS → non-local potential). The Weyl symbol of L diss is
L W [ A W ] = γ n Π n W A W Π n W 1 2 { Π n W Π n W , A W } ,
where Π n W ( x , n ) = δ n n , giving exponential diagonalisation in the internal index.

Proof

Since each Kraus operator is a rank-1 projector, the star product reduces to ordinary matrix multiplication in the irreducible internal index n. □

3.7.4. Lemma 3: Symbol Map of the Zero-Area Kernel [69]

Lemma 29
(Weyl symbol of the Lie flow). The Weyl action of the zero-area kernel R is R W [ A W ] = u a a A W .

Proof

The flow map e ε L u induces a phase-space translation; the limit ε 1 f ( x ε u ) f ( x ) yields the Lie derivative. □

3.7.5. Equivalence Theorem [70]

Lemma 30
(Operator form ⇔ Field-equation form). The Wigner–Weyl transform W and its inverse W 1 mutually map the operator form UEE op (3.2.4) and the field-equation form UEE fld (3.4.5), establishing a bijection.

Proof

(i) op fld : Translate each term of ρ ˙ with Lemmas A198–29. Form the energy–momentum tensor T a b = d 4 p p a p b A W and assemble Einstein’s equation; the scalar equation follows from the u a flow condition.
(ii) fld op : Given a field solution ( g a b , ψ , Φ ) , reconstruct the density operator via Weyl quantisation ρ = W 1 [ A W ] . Linearity of W 1 and closure of the star product ensure the operator form is satisfied.
Surjectivity and injectivity being shown, the mapping is bijective. □

3.7.6. Conclusion

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3.8. Existence-and-Uniqueness Theorem

3.8.1. Functional-analytic framework [71,72]

We regard the density operator as
ρ ( t ) B 1 : = ρ L ( H ) ρ = ρ , ρ 0 , ρ = 1 ,
a Banach space under the trace norm ρ 1 : = | ρ | . The generator L : = ( i ad D ) + L diss + R (eq. (3.2.4)) is a closed operator on B 1 .
Commutative diagram:
B 1 L B 1 C ( [ 0 , T ] , B 1 )
will be used with the Banach fixed-point theorem.

3.8.2. Lemma 1: local Lipschitz continuity [73]

Lemma 31
(Local Lipschitz property). For any bounded set Ω B 1 there exists a constant K Ω such that
L [ ρ 1 ] L [ ρ 2 ] 1 K Ω ρ 1 ρ 2 1 , ρ 1 , 2 Ω .

Proof

The reversible part i [ D , · ] is bounded, [ D , X ] 2 D X . The dissipator is a CPTP linear map and therefore 1-Lipschitz ([466], Thm. 2.1). The zero-area term R = L u generates a strongly continuous one-parameter flow with R [ X ] 1 v 0 X 1 ( v 0 : = sup | u | ). Collecting the constants gives K Ω . □

3.8.3. Lemma 2: global boundedness via dissipation [74]

Lemma 32
(A-priori trace-norm bound). If a solution ρ ( t ) exists for initial datum ρ 0 B 1 , then
ρ ( t ) 1 = 1 , t 0 .

Proof

ρ ˙ = L [ ρ ] = 0 because L diss and R are trace-preserving and [ D , ρ ] is traceless. With ρ 0 = 1 the trace is conserved. □

3.8.4. Local-solution existence [75]

Lemma 33
(Banach fixed-point for local solutions). For any ρ 0 B 1 there exists T > 0 and a unique ρ C ( [ 0 , T ] , B 1 ) solving the integral equation ρ ( t ) = ρ 0 + 0 t L [ ρ ( s ) ] d s .

Proof

Let B R : = { ρ C ( [ 0 , T ] , B 1 ) sup t [ 0 , T ] ρ ρ 0 1 R } , and use Lemma 31 with K : = K B R . Choosing T < R / K makes the Picard map Φ [ ρ ] ( t ) = ρ 0 + 0 t L [ ρ ] d s a contraction on B R ; the Banach fixed-point theorem yields the unique local solution. □

3.8.5. Extension to global solutions [4]

Lemma 34
(Existence of a unique global solution). By Lemmas 32 and 33 the local solution can be uniquely extended to any finite time interval.

Proof

The boundedness ρ ( t ) 1 = 1 excludes blow-up. Repeating the local fixed-point argument on successive intervals extends the solution to [ 0 , ) . □

3.8.6. Existence-and-uniqueness theorem [6]

Lemma 35
(Global solution of the UEE). For any initial datum ρ 0 B 1 , the operator-form UEE (3.2.4) possesses a unique global solution ρ C 1 ( [ 0 , ) , B 1 ) . Moreover, via the Wigner–Weyl transform and the variational principle, corresponding solutions in the variational and field-equation forms exist simultaneously, yielding a triple solution ( ρ , ψ , ψ ¯ , Φ , g a b ) across all three formulations.

Proof

Lemma 34 provides the global solution of the operator form. The equivalence theorems 22, 26, and 30 map this solution bijectively to the variational and field-equation solutions, which are therefore unique as well. □

3.8.7. Conclusion

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3.9. Conserved Quantities and Entropy Production

3.9.1. Conservation of Energy and Charge [53,67]

(i) Energy operator

Identify the reversible generator with the Hamiltonian, H : = D , and define the energy expectation value E ( t ) : = [ ρ ( t ) H ] .
Lemma 36
(Energy conservation law). The time evolution governed by the operator form (3.2.4) satisfies E ˙ ( t ) = 0 .

Proof

E ˙ = [ ρ ˙ H ] = ( i [ H , ρ ] + L diss [ ρ ] + R [ ρ ] ) H . The commutator term gives [ H , [ H , ρ ] ] = 0 . For L diss and R one has [ L diss [ ρ ] H ] = [ ρ L diss [ H ] ] ; by GKLS duality L diss [ H ] = 0 . R is self-adjoint, and [ R [ ρ ] H ] = [ ρ R [ H ] ] = 0 using Lemma 14. Hence E ˙ = 0 . □

(ii) Internal U ( 1 ) charge

Let Q : = n q n Π n be a conserved charge. A calculation analogous to the above shows Q ˙ ( t ) = 0 .

3.9.2. von Neumann entropy and dissipation [48,76]

Define S v N ( t ) : = [ ρ ( t ) ln ρ ( t ) ] .
Lemma 37
(Spohn inequality). For the GKLS dissipator L diss ,
d S v N d t = [ L diss [ ρ ] ln ρ ] 0 .

Proof

L diss is the generator of a trace-preserving completely positive semigroup; Spohn’s inequality ([48], Thm. 1) applies. □
The zero-area flow R contributes [ R [ ρ ] ln ρ ] = [ ρ R [ ln ρ ] ] = 0 by its symmetric self-adjoint structure, so it does not affect the entropy balance.

3.9.3. Universal form of the entropy-production rate [77]

Lemma 38
(Universal entropy production). The entropy-production rate in the single-fermion UEE is
d S v N d t = γ n = 1 18 ( Π n ρ Π n 1 2 { Π n , ρ } ) ln ρ 0
and equality holds only when ρ = n p n Π n , i.e. when ρ is diagonal in the pointer basis.

Proof

Combine Lemma 37 with the rank-1 property of the projectors to write out the integral explicitly. The condition d S v N d t = 0 requires Π n ρ = ρ Π n , implying diagonality. □

3.9.4. Consistency across the three forms [5]

Operator form

Lemmas 36–37 hold directly.

Variational form

Noether current conservation ( T a 0 ) and the positive Kullback–Leibler property of the dissipative functional give the same expressions.

Field-equation form

a T a 0 = 0 and the positivity of J res reproduce the entropy-production law.

3.9.5. Conclusion

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3.10. Summary and Bridge to the Subsequent Chapters

3.10.1. Achievements and Significance of the Three-Form Equivalence

In this chapter we established, line by line,
UEE op UEE var UEE fld ,
i.e. a reversible chain of equivalences. The main results are:
  • Operator form — construction of the unique CPTP quantum dynamics from the five-operator complete set (§3.2);
  • Variational form — definition of the action S UEE with the tetrad e a ( Φ ) μ (§3.3);
  • Field-equation form — reproduction of GR + SM + dissipative sources with zero extra parameters (§3.4);
  • Equivalence proofs — reversible mappings among the three forms using Wigner–Weyl and GNS path integration (§§3.5–3.7);
  • Global existence and uniqueness — ensured by the Banach fixed-point theorem and dissipative boundedness (§3.8);
  • Conservation laws and entropy — consistency between energy conservation and the Spohn inequality (§3.9).

3.10.2. Inter-Chapter Mapping: Which Form to Use?

Table 3. Recommended primary form in each upcoming chapter
Table 3. Recommended primary form in each upcoming chapter
Subsequent chapter Main task Recommended form Rationale
Part II, Chs. 4–6 Microscopic analysis of measurement and thermalisation Operator form Shortest route for decoherence calculations
Part II, Ch. 7 β functions and loop corrections Variational form Symmetry control via covariant action principle
Part III, Chs. 8–10 Yukawa exponential law and mass gap Operator ↔ Variational Projector exponent + Feynman diagrams
Part IV, Chs. 11–13 GR reduction, cosmology, BH information Field-equation form Direct handling of background geometry

3.10.3. Logical Roadmap Going Forward

1
Part II will use the operator form as the base to analyse the measurement problem and dissipative thermalisation rigorously, deriving the Born rule and the Zeno effect.
2
Part III will exploit the variational form and the projector-induced Yukawa matrices to verify numerically the SM mass hierarchy and the precision correction δ ρ vac = 0 .
3
Part IV will employ the field-equation form to recover GR from the Φ -tetrad, derive the modified Friedmann equation, and resolve the BH information issue.

3.10.4. Theoretical and Practical Advantages

  • Freedom of form conversion — analytic, numerical, and interpretational tasks can each use the optimal tool.
  • Elimination of loopholes — identical results in all forms remove dependence on any single representation.
  • Transparency to external researchers — accessible to communities versed in operator theory, field theory, or variational methods.

3.10.5. Conclusion

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4. Real Hilbert Space and Projection Decomposition

4.1. Introduction and Domain Setting

4.1.1. Aims and Position of This Chapter [41,78,79]

In the single-fermion UEE the quantum state space is defined not on a complex Hilbert space H but on an underlying real Hilbert space  H R . The purposes of this chapter are:
* to prove separability and completeness of H R (Section 4.2); * to establish the complexification H R R C H and the C * -representation (Section 4.3); * to construct and prove uniqueness of the 18 one-dimensional projections corresponding to the Standard-Model degrees of freedom (Section 4.4–4.7).
These results lay the groundwork for the measurement theory and dissipative analysis in the subsequent chapters.

4.1.2. Definition of the Real Hilbert Space [6,80,81]

Definition 9
(Real Hilbert space). Let H R be a real vector space equipped with a real inner product · , · R . If H R is complete and separable with respect to · , · R , then H R , · , · R is called areal Hilbert space.
Definition 10
(Complexification). The complexification of H R is defined by
H : = H R R C = { ψ 1 + i ψ 2 ψ 1 , 2 H R } ,
with inner product
ψ 1 + i ψ 2 , ϕ 1 + i ϕ 2 : = ψ 1 , ϕ 1 R + ψ 2 , ϕ 2 R + i ψ 2 , ϕ 1 R ψ 1 , ϕ 2 R ,
turning H into a complex Hilbert space.

4.1.3. Introduction of a Finite-Dimensional Internal Space and Separated Representation [26,42,82]

The internal degrees of freedom of Standard-Model fermions (colour 3 × weak isospin 2 × generation 3) are represented by the finite-dimensional real space R 18 , and we set
H R tot : = H R ( spacetime ) R 18 .
Henceforth the projection family { Π ( α , β , γ ) } 18 will be constructed as one-dimensional projections on this internal space (see Section 4.4 for details).

4.1.4. Notation Adopted in This Chapter [2,83]

  • Real space: H R with elements v , w .
  • Complexification: H with elements ψ , ϕ .
  • Internal indices: α = 1 , 2 , 3 (colour), β = 1 , 2 (weak), γ = 1 , 2 , 3 (generation).
  • The real inner product · , · R and the complex inner product · , · are distinguished by the superscript “ R ’’ where needed.

4.1.5. Conclusion

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4.2. Separability Theorem for the Real Hilbert Space

4.2.1. Concrete Model of the Real Space [10,65]

As the one–particle real state space of the quantum field we adopt
H ( spacetime ) : = { ψ : R 3 R 4 ψ L 2 ( R 3 , R 4 ) , ψ , ϕ R : = R 3 ψ ( x ) · ϕ ( x ) 3 x ,
where “ · ” is the Euclidean inner product in R 4 at each point.

4.2.2. Basic Lemma: Density of Bounded Compact-Support Functions [84,85]

Lemma 39
(Dense set D Q ). Let Q k : = [ k , k ] 3 be bounded closed cubes. Consider finite products of indicator functions χ Q k 1 χ Q k m with coefficients chosen from Q 4 . The linear span of such functions, denoted D Q , is dense in L 2 ( R 3 , R 4 ) .

Proof

Step functions span a dense subspace because smooth compact–support functions can be approximated in the L 2 norm (Stone–Weierstrass plus Morrey’s theorem). Approximating real coefficients by rational numbers yields arbitrary precision, hence D Q is dense. □

4.2.3. Separability Theorem [81,86]

Theorem 14
(Separability of the real Hilbert space). The space H ( spacetime ) is separable; that is, it possesses a countable dense subset.

Proof

The set D Q in Lemma 39 is countable because it is generated by a countable collection of bounded cubes together with coefficients in Q 4 . Since its linear span is dense in L 2 , the space H ( spacetime ) is separable. □

4.2.4. Remark on Completeness [6,81]

Completeness follows because L 2 ( R 3 , R 4 ) is the real part of a Lebesgue space L 2 , known to be complete ([467], Thm. 3.14).

4.2.5. Conclusion

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4.3. Complexification and C * -Algebra Representation

4.3.1. Rigorous Definition of the Complexification [8,87]

Definition 11
(Complexification (recalled)). For a real Hilbert space H the complexification is
H C : = H R C = { ψ 1 + i ψ 2 ψ 1 , 2 H ,
endowed with the inner product
ψ , ϕ : = ψ , ϕ R + ψ , ϕ R + i ψ , ϕ R ψ , ϕ R .
Lemma 40
(Preservation of separability). If H is separable, then H C is also separable.

Proof

Take a countable dense set { v k } H ; then { v k , i v k } is countable and dense in H C . □

4.3.2. Bounded-Operator Algebra and the C * Norm [46,88]

Definition 12
(Algebra of bounded operators). Denote by B ( H C ) the *-algebra of bounded linear operators on H C equipped with the operator norm A : = sup ψ = 1 A ψ .
Lemma 41
( C * identity). In B ( H C ) one has A * A = A 2 ; hence B ( H C ) is a C * -algebra.

4.3.3. Correspondence between Real and Complex Operators [6,89]

Definition 13
(Complex lift of a real operator). For T B ( H ) the complex lift T C B ( H C ) is defined by T C ( ψ 1 + i ψ 2 ) : = T ψ 1 + i T ψ 2 .
Lemma 42
(Isometric *-monomorphism). The map L : B ( H ) B ( H C ) , T T C , is a *-algebra monomorphism and satisfies T C = T .

Proof

Linearity and ( T C ) * = ( T * ) C follow by inspection. For norm preservation note T C ψ 2 = T ψ 2 + T ψ 2 T 2 ψ 2 , and equality is attained on a real vector. □

4.3.4. GNS Representation of a C * Algebra [90,91]

Definition 14
(State). Astateis a normalized positive functional ω : B ( H C ) C obeying ω ( A A * ) 0 and ω ( 1 ) = 1 .
Theorem 15
(GNS construction (complex version)). For every state ω there exists a unique (up to unitary equivalence) triple ( π ω , H ω , | Ω ω ) such that ω ( A ) = Ω ω | π ω ( A ) | Ω ω .

Proof

Apply the standard GNS construction ([8], Thm. 10.2.4) in the complex space H C ; the real–to–complex lift incurs no inconsistency. □

4.3.5. Inclusion of the Real Operator Algebra into a C * Algebra [8,10]

Theorem 16
(Real C * embedding theorem). The operator algebra B ( H ) is embedded via the isometric *-monomorphism L as a C * sub-algebra of B ( H C ) .

Proof

Lemma 42 shows that L is a *-algebra monomorphism preserving the C * identity, hence the C * -norm closure coincides with its image. □

4.3.6. Conclusion

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4.4. Construction of the Projection Family: Gram–Schmidt 18-Basis

4.4.1. Tensor-Product Space of Internal Degrees of Freedom [92,93]

H int : = C color 3 C weak 2 C gen 3 C 18 .
Convention: c = 1 , 2 , 3 (colour), w = 1 , 2 (weak isospin), gen = 1 , 2 , 3 (generation).

4.4.2. Gram–Schmidt Orthonormal Basis [94,95]

Definition 15
(Initial product basis). The natural basis | c c | l w | g gen is abbreviated as | c w gen .
The product basis is already orthogonal, but for completeness we apply the Gram–Schmidt procedure once.

Algorithm (sketch)

| e 1 : = | 111 , | e 2 : = | 121 e 1 | 121 | e 1 N 2 , , | e 18 : = orthonormalized | 333 .
Since e i | j k l = δ i j , k l , one finds N k = 1 . Hence
| e n = | c w gen , n ( c , w , gen ) .

4.4.3. Definition of One-Dimensional Projections [78,96]

Definition 16
(Internal pointer projections).
Π ( c , w , gen ) : = | e ( c , w , gen ) e ( c , w , gen ) | , n ( c , w , gen ) { 1 , , 18 } .
Lemma 43
(Orthogonality). Π n Π m = δ n m Π n .

Proof

Insert the basis orthogonality e n | e m = δ n m . □
Lemma 44
(Completeness). n = 1 18 Π n = 1 H int .

Proof

The set { | e n } is a complete orthonormal basis of H int . □

4.4.4. Tensor Projection with the External Space [97,98]

For the total Hilbert space H C tot : = H C ( spacetime ) H int define
Π n tot : = 1 H C ( spacetime ) Π n , n = 1 , , 18 ,
which act on the internal indices while leaving the spatial degrees of freedom untouched.

4.4.5. Physical Labels of the Projection Family [2,42]

n ( colour c , weak w , gen gen ) .
Thus a single-fermion internal state ψ ( x ) expands as ψ ( x ) = n = 1 18 ψ n ( x ) | e n , with each component ψ n ( x ) corresponding to a Standard-Model fermion ( q colour , l weak ) .

4.4.6. Conclusion

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4.5. Orthogonality and Completeness Theorem for the Projection Family

4.5.1. Recap of the Definition [96,99]

The one–dimensional projections constructed in Section 4.4 are Π n = | e n e n | , n = 1 , , 18 , where | e n are the Gram–Schmidt 18 basis vectors.

4.5.2. Rigorous Proof of Orthogonality [100]

Lemma 45
(Orthogonality). For any n m   Π n Π m = 0 , Π n 2 = Π n .

Proof

Using the basis orthogonality e n | e m = δ n m ,
Π n Π m = | e n e n | e m e m | = δ n m | e n e m | .
Hence for n m we obtain the zero operator. Moreover, Π n 2 = | e n e n | e n e n | = Π n .

4.5.3. Rigorous Proof of Completeness [80,101]

Lemma 46
(Completeness).
n = 1 18 Π n = 1 H int .

Proof

The 18 basis vectors form a complete orthonormal basis of H int . For any | ψ H int , | ψ = n e n | ψ | e n = n Π n | ψ . Therefore n Π n = 1 . □

4.5.4. Uniqueness of the Minimal Complete Projection Family [102,103]

Theorem 17
(Minimality and Uniqueness). The set Π set constitutes theminimalfamily of one–dimensional orthogonal projections spanning H int with exactly 18 members, and any other such family is unitarily equivalent to it.

Proof

Let d : = dim H int = 18 . Because the image of each orthogonal one–dimensional projection is one–dimensional, at least d projections are required for completeness. Lemma 46 shows that Π set attains completeness with d projections, hence 18 is minimal. By the spectral theorem, any two complete sets of rank-1 orthogonal projections are related by a unitary basis transformation; no non-unitary equivalence exists. □

4.5.5. Conclusion

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4.6. Mapping from the Real Orthogonal Basis to the Pointer Basis

4.6.1. Complex Extension of the Real Orthogonal Basis [10]

{ v k } k N H ( spacetime ) countable orthonormal basis { v k , i v k } k N is dense in H C ( spacetime ) .
Tensoring with the Gram–Schmidt 18 internal basis | e n (§4.4) we obtain
| v k | e n ( k N , n = 1 , , 18 )
as a countable orthogonal basis of H C tot : = H C ( spacetime ) H int .

4.6.2. Internal Observable Defining the Pointer Basis [30,104]

Definition 17
(Internal Cartan observable). The self-adjoint operator acting on the internal degrees of freedom
O : = n = 1 18 λ n Π n , λ n : = 3 2 ( color ) + 2 ( weak ) + gen ,
is called the pointer Hamiltonian. Here Π n are the projections of §4.4.
Lemma 47
(Spectral decomposition). The operator O has non-degenerate eigenvalues λ n and the corresponding eigenprojections are Π n .

Proof

Each eigenvector satisfies O | e n = λ n | e n . Because the eigenvalues are distinct integers, no degeneracy occurs; each eigenspace is one-dimensional. □

4.6.3. Unitary Map from the Real Basis to the Pointer Basis [3,105]

Theorem 18
(Uniqueness of the pointer-unitary map). For any real orthonormal basis { | v k } H C ( spacetime ) and the internal basis { | e n } H int , the total-space basis | v k | e n can be mapped to the pointer basis
| x , k , n ptr : = | x | v k | e n , x R 3 ,
by a unitary operator U , which is unique up to a diagonal phase matrix diag ( e i θ k n ) .

Proof

By the spectral theorem (Lemma 47), O = n λ n Π n is diagonalised by a unitary that preserves the images of Π n :
U = k , n e i θ k n | x , k , n ptr x , k , n | .
Because each eigenspace is one-dimensional, only the phases e i θ k n remain as free parameters. □

4.6.4. Pointer Expansion and Phase Freedom [106,107]

| Ψ = k , n 3 x Ψ k n ( x ) U | x , k , n real .
The phases e i θ k n do not appear in physical observables; only the Born probabilities | Ψ k n ( x ) | 2 contribute to experimental outcomes.

4.6.5. Conclusion

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4.7. Spectral Theorem and Uniqueness of the Projection Decomposition

4.7.1. Scope of the Spectral Theorem [103,108]

Recall that the self-adjoint operator O , acting only on the finite-dimensional internal space H int , is already diagonalised,
O = n = 1 18 λ n Π n , ( λ n R , Π n 2 = Π n ) .
In what follows we establish, as a theorem, why this projection decomposition is unique.

4.7.2. Uniqueness Lemma for the Spectral Measure [109]

Lemma 48
(Uniqueness of a finite spectral measure). On a finite-dimensional Hilbert space dim H int = 18 , let O be a self-adjoint operator with a set ofdistincteigenvalues { λ n } . Then the spectral measure E ( Δ ) is uniquely determined by E ( { λ n } ) = Π n .

Proof

The spectral measure E assigns a projection to every Borel set Δ R and satisfies O = R λ E ( λ ) . Because the eigenvalues are non-degenerate, λ n λ m for n m , the supports Δ n : = { λ n } are disjoint. By uniqueness of the spectral decomposition we have E ( Δ n ) = Π n as the only possible solution. □

4.7.3. Uniqueness of the Projection via Unitary Equivalence [110]

Lemma 49
(Uniqueness theorem for projection decompositions). Suppose that O = n λ n Π n = m μ m Π ˜ m admits two spectral decompositions. As long as the eigenvalues are non-degenerate,
U U ( H int ) such that Π ˜ m = U Π σ ( m ) U ,
where σ is a permutation aligning the order of the eigenvalues. Hence the set of projections is unique up to unitary equivalence.

Proof

By Lemma 48 the projection corresponding to each eigenvalue is unique: Π n = E ( { λ n } ) . In the alternative decomposition the projection with the same eigenvalue is denoted Π ˜ σ ( n ) (after re-ordering). Because each eigenspace is one-dimensional, define unitary maps U n : Π n H int Π ˜ σ ( n ) H int , free only up to an overall phase. Taking their direct sum U : = n U n gives Π ˜ σ ( n ) = U Π n U . No other freedom remains than these phases. □

4.7.4. Implications for the Pointer Hamiltonian [3,111]

For the pointer operator O = n λ n Π n (§4.5) all eigenvalues λ n are distinct integers. Therefore Theorem 49 applies directly, showing that the pointer basis and its projection family are unique up to phase factors.

4.7.5. Conclusion

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4.8. Physical Correspondence of the 18-Dimensional Internal Space

4.8.1. Projection Labels and Standard-Model Fermions [42,92]

The Gram–Schmidt 18 basis | e ( α , β , γ ) ( α = 1 , 2 , 3 ; β = 1 , 2 ; γ = 1 , 2 , 3 ) is labelled as
α colour ( r , g , b ) , β weak ( L , R ) , γ generation ( 1 , 2 , 3 ) .
n α β γ Physical particle (charge Q)
1–3 r , g , b L 1 up quark u L ( + 2 3 )
4–6 r , g , b R 1 up quark u R ( + 2 3 )
7–9 r , g , b L 1 down quark d L ( 1 3 )
10–12 r , g , b R 1 down quark d R ( 1 3 )
13 L 1 electron e L ( 1 )
14 R 1 electron e R ( 1 )
15 L 1 neutrino ν L (0)
16–18 same 2,3 generational replicas
Only the first generation is detailed here for brevity. The label assignment is n = 9 ( γ 1 ) + 3 ( β 1 ) + α .

4.8.2. Internal Representation of the Charge Operator [112,113]

Definition 18
(Internal charge operator).
Q : = α , β , γ q α β Π ( α , β , γ ) , q r L = + 2 3 , q r R = + 2 3 , q g L = + 2 3 ,
where the right-hand side runs over α = r , g , b and β = L , R .
Lemma 50
(Charge eigen-projections). Q Π n = q n Π n , where q n equals the charge values in the table above.

Proof

The operator Q is diagonal in the projection decomposition. Using Π m Π n = δ m n Π n the statement follows immediately. □

4.8.3. Correspondence Between Labels and Gauge Group [26,114]

Lemma 51
(Action of SU ( 3 ) × SU ( 2 ) × U ( 1 ) ). The gauge action U colour U weak e i θ Q preserves each projection Π ( α , β , γ ) and thus retains orthogonality and completeness.

Proof

U colour acts on the colour index α , while U weak rotates the weak index β ; the two act in tensor product, and e i θ Q is diagonal. Hence at the operator level U Π n U = Π m , where m has the same ( β , γ ) but a permuted α . Projection properties are unchanged. □

4.8.4. Physical Projection Theorem [115,116]

Lemma 52
(One-to-one correspondence between internal projections and SM fermions). The projection Π ( α , β , γ ) carries no orbit under the gauge action of Lemma 51; its one-dimensional range is uniquely isomorphic to the Standard-Model fermion eigenstate ψ α β γ SM ( x ) .

Proof

The gauge action merely rotates the internal indices and preserves the projection ranges. Because the eigenvalues (charge, weak T 3 , etc.) are non-degenerate, each projection coincides with the corresponding eigenstate space; hence the correspondence is unique. □

4.8.5. Conclusion

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4.9. Conclusion and Bridge to Chapter 5

Starting from the real Hilbert space we have shown:
(i)
Separability and completeness A rigorous Banach–basis proof that the real L 2 space possesses a countable dense subset (Section 4.2).
(ii)
Complexification and C * -algebra The real operator algebra B ( H ) is isometrically embedded into B ( H C ) ; every state has a unique GNS representation (Section 4.3).
(iii)
Construction of the projection family Π set From the Gram–Schmidt 18 basis we built one-dimensional orthogonal projections and proved orthogonality, completeness and minimal uniqueness (Section 4.4–4.6).
(iv)
Isomorphism with physical degrees of freedom Each projection Π n is put in one-to-one correspondence with ( colour , weak , generation ) , thereby encompassing all Standard-Model fermions (Section 4.7).

1. Diagonalisation for the Born rule

The dissipative jump operators V n = γ Π n (Chapter 2), together with the now fixed Π n , instantaneously diagonalise the density operator, yielding the measurement probabilities Prob ( n ) = [ ρ Π n ] (Chapter 5, §§5.1–5.2).

2. Exact evaluation of the Spohn inequality

The entropy production rate S ˙ = [ L diss [ ρ ] ln ρ ] closes in the Π n basis, permitting analytic calculation of the quantum Zeno effect and thermalisation time (Chapter 5, §5.3).

3. S-matrix and β -function

The tensor-product projections map the internal indices of scattering states explicitly to particle labels; S-matrix elements containing projection sums become finitely renormalisable (Chapter 5, §5.4).
  • Chapter 5 starts from the Π n diagonalisation to derive the Born rule and a measurement theory.
  • From Chapter 6 onward, the pointer basis is used for entanglement entropy and optimal evaluation of the Spohn inequality.
  • In Chapter 8 the labelling established here enters the concrete determination of coefficients in the Yukawa scaling m f ε O f .

4.9.1. Conclusion

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5. Measurement and Dissipative Diagonalisation of the Born Rule

5.1. Introduction and Problem Setting

5.1.1. Objectives of This Chapter [30,78,79]

Using the uniquely fixed internal projection family from Chapter 4,
Π set : = { Π n } n = 1 18 , V n = γ Π n
(the jump operators of Chapter 2, §2.4), we aim to:
1
Derive the quantum–measurement probability law (the Born rule) as a dissipative diagonalisation process.
2
Obtain the decoherence time t dec = γ 1 in a natural way.
3
Analyse the conditions for measurement back-action and the quantum Zeno effect.

5.1.2. Difference from the Conventional Measurement Postulates [100,117,118]

In orthodox quantum mechanics the projection-postulate (state reduction) is introduced axiomatically. Within the single-fermion UEE:
  • The dynamics is always CPTP and continuous: ρ ˙ contains no instantaneous projection.
  • Measurement appears as the short-time limit of the dissipative semigroup exp ( t L diss ) generated by the V n .
Demonstrating this structure analytically is the task of the present chapter.

5.1.3. Notation and Working Assumptions [15,17,119]

Definition 19
(Initial density operator). ρ 0 B 1 H C tot may be any pure or mixed state.
Definition 20
(Dissipative generator).
L diss [ ρ ] = γ n = 1 18 Π n ρ Π n 1 2 { Π n , ρ } .
Lemma 53
(Commutativity). The generator L diss commutes with every pointer operator Π m : L diss [ Π m ] = 0 .

Proof

A direct calculation of the commutator shows that each term contains Π m twice; the result is zero. □
Working assumption: in this chapter we neglect the reversible generator D and the zero-area kernel R on the short time-scale and investigate the leading effect of the dissipator only.

5.1.4. Conclusion

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5.2. Dissipative Jump Operators and Instantaneous Diagonalisation

5.2.1. Formal Solution of the Dissipative Semigroup [15,119,120]

From the jump operators V n = γ Π n the generator is
L diss [ ρ ] = γ n = 1 18 Π n ρ Π n 1 2 { Π n , ρ } ,
and the corresponding Lindblad semigroup is ρ ( t ) = e t L diss ρ 0 . By the commutativity Lemma  53 L diss preserves the Π n blocks.

5.2.2. Exponential Decay of Off-Diagonal Terms [3,111,121]

Lemma 54
(Suppression of off-diagonals). Decompose the initial state as ρ 0 = ρ diag + ρ o f f with ρ diag : = n Π n ρ 0 Π n and ρ o f f : = ρ 0 ρ diag . Then
e t L diss ρ 0 = ρ diag + e γ t ρ o f f .

Proof

For each matrix element ρ n m : = Π n ρ Π m ( n m ) we have ρ ˙ n m = γ ρ n m by direct computation. Solving with the initial condition gives ρ n m ( t ) = e γ t ρ n m ( 0 ) . Diagonal elements satisfy ρ ˙ n n = 0 . Combining both parts yields the stated formula. □

5.2.3. Theorem of Instantaneous Diagonalisation [48,122]

Theorem 19
(Instantaneous diagonalisation by dissipation). On the time scale t γ 1 ,
ρ ( t ) γ t 1 ρ diag = n = 1 18 Π n ρ 0 Π n ,
i.e. the state becomes fully diagonal in the pointer basis.

Proof

In Lemma 54 the off-diagonal terms vanish exponentially as e γ t 0 for γ t 1 . □

5.2.4. Physical Meaning—The Pre-measurement State [104,123,124]

The dissipation rate γ is proportional to the system–environment coupling strength, and t dec = γ 1 is the decoherence time. For t t dec the state read out by the measuring device is restricted to ρ diag .

5.2.5. Conclusion

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5.3. Derivation of the Born Rule

5.3.1. State Description Before and After Measurement [96,125]

From the dissipative–diagonalisation theorem (Theorem 19) we have, for t γ 1 ,
ρ ( t ) = ρ D = n = 1 18 p n Π n , p n : = Tr [ Π n ρ 0 ] .
The set { p n } is positive and satisfies n p n = 1 by trace preservation.

5.3.2. Proof of the Probability Law [100,126,127]

Lemma 55
(Normalisation of probabilities). One has p n 0 and n p n = 1 .

Proof

Because Π n is a positive projection, Π n ρ 0 Π n 0 ; trace positivity yields p n 0 . Completeness n Π n = 1 together with Tr ρ 0 = 1 implies n p n = 1 . □
Theorem 20
(Born rule (UEE version)). The probability of obtaining the measurement outcome n in the pointer basis is
P ( n ) = Tr [ ρ 0 Π n ]

Proof

Immediately before read-out the state is ρ D ; for a projective measurement the probability is P ( n ) = Tr [ ρ D Π n ] . Since ρ D Π n = p n Π n and Tr [ Π n ] = 1 (one–dimensional projection), P ( n ) = p n = Tr [ Π n ρ 0 ] . □

5.3.3. Post-Measurement State (Lüders Update) [96,128]

Stopping the dissipative semigroup at a small time δ t before t gives the conditional state
ρ n | δ t = Π n ρ ( δ t ) Π n Tr [ Π n ρ ( δ t ) ] δ t 0 Π n ρ 0 Π n p n ,
which coincides with the standard Lüders rule.

5.3.4. Recovery of Expectation Values [129,130]

For any observable A commuting with all Π n
A after = n p n Tr A Π n = Tr [ A ρ 0 ] ,
showing that no statistical bias is introduced by the measurement.

5.3.5. Conclusion

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5.4. Dissipative Time-scale and Decoherence

5.4.1. Time Evolution of the Off-Diagonal Fidelity [3,111]

Tracing the result of Theorem 19 at the level of matrix elements, for indices n m we have
C n m ( t ) : = Tr Π n ρ ( t ) Π m = C n m ( 0 ) e γ t ,
where C n m ( 0 ) is the initial coherence.

5.4.2. Definition of the Decoherence Time [17,121]

Definition 21
(Decoherence time).
t dec : = γ 1 ln 1 ϵ ,
with a small threshold ϵ 1 such that coherence is deemed practically vanished if | C n m ( t dec ) | ϵ | C n m ( 0 ) | .
Choosing, in particular, ϵ = e 1 yields the natural-unit decoherence time  t dec = γ 1 .

5.4.3. Diverging Entropy and the Spohn Inequality [48,131]

Lemma 56
(Growth rate of the linear entropy). For the linear entropy S 2 : = 1 Tr [ ρ 2 ] one has
d S 2 d t = 2 γ n m | C n m ( t ) | 2 0 .

Proof

Using ρ ˙ = γ ρ o f f + and evaluating Tr [ ρ ρ ˙ ] . Only off-diagonal elements contribute; insert equation (5.3.1). □
The result is compatible with the Spohn inequality S ˙ vN 0 (Chapter 3, §3.9); S 2 saturates rapidly on the scale t dec .

5.4.4. Physical Model for the Parameter γ [132,133]

For a weakly coupled linear system–environment model
V int = n A n B n , A n = | e n e n | ,
a Redfield/GKLS reduction gives γ = 2 π J ( ω = 0 ) | g | 2 , where J ( ω ) is the environmental spectral density and g the coupling constant. Hence
t dec 1 | g | 2 J ( 0 ) .

5.4.5. Illustrative Experimental Values [123,134,135]

In laser-cooled atomic systems with | g | 10 2 MHz and J ( 0 ) 10 3 Hz , t dec 10 5 s . In high-temperature solids the time can shrink down to the femtosecond regime.

5.4.6. Conclusion

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5.5. Quantum-Zeno Effect and the Continuous-Measurement Limit

5.5.1. Set-up of the Discrete-Measurement Protocol [136,137]

Definition 22
(Discrete measurement sequence). The total observation time T is divided into N equal intervals, giving the inter-measurement spacing τ M = T / N . During each interval we apply, in alternation,
  • the dissipative semigroup evolution exp ( τ M L diss ) , and
  • the projective measurement { Π n } .
We denote the overall operation by M N .
For an initial state ρ 0
ρ ( N ) ( T ) : = n Π n e τ M L diss N ρ 0 m e τ M L diss Π m N .

5.5.2. Zeno Contraction Lemma [138,139]

Lemma 57
(Low-order transition probability). If τ M γ 1 , the off-diagonal transition probability is
P n m ( τ M ) = γ τ M + O ( γ τ M ) 2 , ( n m ) .

Proof

Expand exp ( τ M L diss ) ρ = ρ + τ M L diss [ ρ ] + O ( τ M 2 ) . For n m , the off-diagonal component of L diss is γ ρ n m (Lemma 54), so the leading transition probability is γ τ M . □

5.5.3. Continuous-Measurement Limit [140,141]

Theorem 21
(Quantum-Zeno fixation theorem). In the limit N , τ M = T / N 0 one obtains
ρ ( N ) ( T ) SOT n Π n ρ 0 Π n ρ diag ,
i.e. the state freezes completely in the pointer-projection subspace.

Proof

The off-diagonal survival factor per measurement step is 1 γ τ M + O ( ( γ τ M ) 2 ) ; after N steps ( 1 γ τ M ) N N e γ T 0 . Lemma 57 shows that the diagonal blocks are preserved while the off-diagonals decay exponentially. The convergence holds in the strong-operator topology (SOT). □

5.5.4. Implications for Measurable Quantities [137,142]

  • Raising the measurement frequency ( τ M 1 ) prolongs the dwell time in a single projection sector; formally τ M 0 yields complete freezing (the Zeno fixation).
  • Practical limitation: if τ M becomes shorter than the detector-response time, apparatus noise effectively increases γ and the Zeno effect is destroyed.

5.5.5. Conclusion

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5.6. Entanglement Generation and Measurement Back-Action

5.6.1. Measurement-apparatus model [78,143]

Definition 23
(Apparatus Hilbert space and pointer states). The measuring device is described by a countable–dimensional Hilbert space H app that possesses mutually orthogonal pointer states { | n app } n = 1 18 . The initial apparatus state is ρ app ( 0 ) = | 0 0 | .
Definition 24
(System–apparatus interaction). The measurement process is realised by the unitary
U meas = n Π n U n , U n | 0 app = | n app ,
i.e. a von-Neumann–type pre-measurement.

5.6.2. Entanglement–generation lemma [144]

Lemma 58
(System–apparatus entangled state). For an initial product state ρ sys ρ app ( 0 ) , the interaction (5.5.1) produces
ρ sys A = n , m Π n ρ sys Π m | n m | app .

Proof

Insert U meas explicitly: U meas ( ρ sys | 0 0 | ) U meas = n , m Π n ρ sys Π m | n m | app . □

5.6.3. Measurement back-action and the Lüders update [130,145]

Theorem 22
(Conditional state update). If the apparatus registers the outcome n, the conditional state of the system is
ρ sys | n = Π n ρ sys Π n Tr [ Π n ρ sys ] ,
i.e. exactly Lüders’ rule.

Proof

The conditional state is ρ sys | n = Tr app [ ( 1 | n n | ) ρ sys A ] / Pr ( n ) . Substituting (5.5.2) and using Pr ( n ) = Tr [ Π n ρ sys ] gives the stated expression. □

5.6.4. Consistency with dissipative diagonalisation [104,146]

In the short-time limit of the dissipative semigroup the system density operator becomes ρ sys ρ diag (Section 5.2). Applying U meas afterwards one has Π n ρ diag Π n = Π n ρ sys Π n ; the entangling unitary therefore merely transfers the classical probabilities to the pointer while leaving the already diagonalised ρ diag unchanged—so the back-action is effectively null.

5.6.5. Entanglement entropy [147,148]

After the pre-measurement, but before reading the pointer (trace over the apparatus),
S vN ( ρ sys ) S vN ( ρ sys A ) = H ( { p n } ) ,
where H is the Shannon entropy. Thus the measurement transfers information to the pointer and can decrease the entropy of the system alone.

5.6.6. Conclusion

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5.7. Extension to General POVMs

5.7.1. Construction principle for POVM elements [11,12]

Starting from the pointer projection family { Π n } we form linear combinations with an Orthon–type coefficient matrix C = ( c μ n ) :
E μ : = n = 1 18 c μ n Π n , c μ n 0
Definition 25
(Projection-sum POVM). If the coefficient matrix satisfies μ c μ n = 1 for every n, the collection { E μ } μ = 1 M is called aprojection-sum POVM.

5.7.2. Completeness and positivity [101,129]

Lemma 59
(POVM completeness).
μ = 1 M E μ = n μ c μ n Π n = n Π n = 1 .

Proof

The first equality is the definition, the second follows from μ c μ n = 1 , and the third from the completeness of { Π n } . □
Because each E μ is a positive linear combination of projections, one has E μ 0 automatically.

5.7.3. Choice of Kraus operators [11,149]

M μ n : = c μ n Π n E μ = n M μ n M μ n .
This “visible’’ dilation is completed entirely within the internal index space—no additional Hilbert space for an environment is required (no Naimark extension).

5.7.4. Measurement probabilities and Lüders update [96,128]

Theorem 23
(POVM probability and state update). For a system state ρ one has
Pr ( μ ) = Tr [ ρ E μ ] , ρ ρ μ = n M μ n ρ M μ n Pr ( μ ) = n c μ n Π n ρ Π n Pr ( μ ) .
In particular, choosing c μ n = δ μ n recovers projective measurement and the usual Born rule.

Proof

Standard GKLS/Kraus construction. Off-diagonal terms Π n ρ Π m ( n m ) vanish because Π n M μ k = 0 unless n = k . Consequently the update involves only projection sums and preserves the pointer-diagonal structure. □

5.7.5. Information–theoretic implications [150,151]

A POVM coarsens the projection information Π n to produce a classical probability distribution p μ = n c μ n p n , whose Shannon entropy satisfies H ( { p μ } ) H ( { p n } ) . The information loss is governed by the mixing properties of the coefficient matrix.

5.7.6. Conclusion

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5.8. Summary and Bridge to Chapter 6

  • Dissipative–diagonalisation theorem (Sec. 5.2): The jump operators V n = γ Π n exponentially diagonalise the density operator ρ in the pointer basis within the time scale t dec = γ 1 .
  • Born rule (Sec. 5.3): After diagonalisation the measurement probabilities appear automatically as P ( n ) = Tr [ ρ 0 Π n ] ; the post–measurement state reproduces the Lüders rule.
  • Quantum Zeno effect (Sec. 5.4): In the limit of vanishing measurement interval τ m 0 the off–diagonal transition amplitudes are suppressed to O ( γ τ m ) , freezing the evolution within the pointer subspace.
  • POVM extension (Sec. 5.6): Any general measurement can be realised as a non–negative coefficient sum E μ = n c μ n Π n that satisfies completeness and positivity, thus eliminating the need for an additional Naimark dilation.

Deterministic core vs. stochastic output

The UEE equation of motion
ρ ˙ = i [ D , ρ ] + L diss [ ρ ] L u ρ
is fully deterministic once the five–operator complete set is specified. Probabilities emerge only at the instant of observation through the two–step mechanism “dissipative diagonalisation projection read-out.’’ Thus quantum probabilities are not intrinsic to the dynamics but are a by–product of the measurement process.

From the Spohn inequality to the area law

The pointer–diagonal state ρ diag obtained after measurement represents a “classicalised’’ quantum state; during thermalisation one has the monotonic approach S v N ( ρ ) t H ( { p n } ) governed by the Spohn inequality. Chapter 6 will analyse
1
the entanglement entropy obeying the area law S e n t A ;
2
the hierarchy between the decoherence time t dec and the thermalisation time t th ;
3
the conditions under which the Zeno effect slows down the thermalisation rate.

Conclusion

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6. Entanglement, Thermalisation, and the Quantum Zeno Effect

6.1. Introduction and Scope

6.1.1. Aims of this chapter [3,30,48]

Building on the dissipative diagonalisation ρ P ptr and the probabilistic measurement framework established in Chapter 5, the goals of the present chapter are:
1
to give a rigorous proof of the area law for the entanglement entropy generated by a pointer–diagonal state, S ent A (Sec. 6.2);
2
to derive a finite–time thermalisation theorem from the Spohn inequality S ˙ v N 0 (Sec. 6.3);
3
to evaluate the hierarchy between the decoherence time t dec and the thermalisation time t th , and to analyse the parameter region in which Zeno-frequency measurements suppress thermalisation (Secs. 6.4–6.5);
4
to ensure that no violation of the area law occurs by invoking bounds on information propagation based on the Lieb–Robinson velocity (Sec. 6.6).

6.1.2. Definitions of the relevant time scales [17,132]

Definition 26
(Decoherence time). Via the dissipative rate γ we set
t dec : = γ 1 ln 1 / ϵ ,
where ϵ 1 denotes the threshold below which coherence is regarded as practically lost (Sec. 5.4). With the representative choice ϵ = e 1 one has t dec = γ 1 .
Definition 27
(Thermalisation time). Depending on the system–environment coupling constant g and on the environmental spectral density J ( 0 ) , we define
t th : = 1 | g | 2 J ( 0 ) .
For many physical systems one finds the hierarchy t dec t th (UEE_02 §9). The analyses in this chapter are carried out under this assumption.

6.1.3. Area law and the pointer basis [111,152,153,154]

Definition 28
(Area law for entanglement entropy). For a spatial region Ω with boundary area  A , the entanglement entropy of the pointer–diagonal state  P ptr is said to obey the “area law’’ if
S ent ( Ω ) = κ A + o ( A ) ,
where the constant κ coincides with the exponential decay rate of the zero-area resonance kernel R and with the structure-formation constant (UEE_02 §9).

6.1.4. Methodological tools employed in this chapter [15,155,156,157]

  • Dissipative master equation: Redfield → GKLS coarse-graining is used to obtain analytic expressions for ρ ( t ) .
  • Information measures: We employ the von Neumann entropy S v N and the relative-entropy production rate.
  • Lieb–Robinson bound: A finite velocity v LR for information propagation is used to control correlation spread.

Conclusion

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6.2. Entanglement Structure of the Pointer-Diagonal State

6.2.1. Form of the pointer-diagonal state [30,121]

From Chapter 5 the pointer-diagonalised state is
P ptr = n = 1 18 D [ ψ n ] P n [ ψ n ] | ψ n ψ n | Π n ,
where the set { | ψ n } lives in the spatial sector H C ( spacetime ) and is tensored with the internal projection Π n .

6.2.2. Definition of the entanglement entropy [2,158]

Definition 29
(Bipartition and entanglement entropy). For a finite spatial region Ω R R 3 with complement Ω C we introduce the tensor decomposition H C ( spacetime ) = H C , Ω R H C , Ω C . Because the pointer projectors act only on the internal space they commute with this split. Tracing over Ω C gives the reduced state P ptr , Ω R : = Tr Ω C P ptr . Its von Neumann entropy S ent ( Ω R ) : = Tr Ω R [ P ptr , Ω R ln P ptr , Ω R ] is called theentanglement entropy.

6.2.3. Clustering lemma [159,160]

Lemma 60
(Exponential clustering induced by the zero-area kernel). The zero-area resonance kernel R induces a finite correlation length ξ such that for two points x , y at distance d ξ one has
Π n ( x ) Π m ( y ) Π n ( x ) Π m ( y ) C 0 e d / ξ .

Proof

The exponential suppression R e A / R generates in the Euler–Lagrange equations a mass term m ξ 1 , leading to a Yukawa-type decay of the two-point function. □

6.2.4. Area-law theorem [152,153,154]

Theorem 24
(Area law for the pointer-diagonal state). Provided the correlation length ξ is finite, the entanglement entropy of the region Ω R satisfies
S ent ( Ω R ) = κ A ( Ω R ) + O ξ A ,
with κ = n p n ln p n , p n = [ Π n P ptr ] .

Proof

Apply the strong sub-additivity  S A B + S B C S A B C S B 0 to adjacent blocks ( A , B , C ) . Lemma 60 bounds long-range contributions by O ( e d / ξ ) . Tiling the global region with cells of width  ξ reduces the entropy to a sum over boundary cells; the number of such cells is proportional to A / ξ 2 , hence the leading area term. Curvature-related corrections are bounded by O ( ξ A ) . □

6.2.5. Physical meaning of the constant κ [37,161]

The constant κ equals the Shannon entropy density of the pointer probabilities,
κ = n p n ln p n = H { p n } ,
quantifying the local degree of mixing. Throughout this chapter the distribution { p n } is assumed to have been equilibrated by the zero-area kernel, so that κ behaves as a universal constant.

Conclusion

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6.3. Spohn’s Inequality and the Thermalisation Theorem

6.3.1. Recap of Spohn’s inequality [15,48]

Definition 30
(Spohn’s inequality). Let a Lindblad semigroup ρ ˙ = L [ ρ ] admit a stationary state ρ eq with L [ ρ eq ] = 0 . Then the relative entropy S ( ρ ρ eq ) = Tr ρ ln ρ ln ρ eq satisfies
d d t S ρ ρ eq = Tr L [ ρ ] ln ρ ln ρ eq 0 .
Throughout this subsection we identify L = L diss and ρ eq = P ptr .

6.3.2. Monotonicity of the relative entropy [162,163]

Lemma 61
(Monotonicity). For ρ ( t ) = e t L diss ρ 0 one has
d d t S ρ ( t ) P ptr 0 , t 0 .

Proof

Since L diss [ P ptr ] = 0 (Sec. 5.2) and L diss is a GKLS generator, the statement follows directly from (6.3.1). □

6.3.3. Thermalisation theorem [164,165,166]

Theorem 25
(Finite-time thermalisation). The relative entropy satisfies
S ρ ( t ) P ptr S ρ 0 P ptr e 2 γ t ,
so that lim t ρ ( t ) = P ptr with exponential rate γ.

Proof

Using the off-diagonal suppression ρ off ( t ) = e γ t ρ off ( 0 ) (Lemma 5.2) we split the relative entropy into diagonal/off-diagonal parts:
S ( ρ P ptr ) = Tr ρ diag ln ρ diag ρ ln P ptr + Tr ρ off ln ρ diag .
The off-diagonal contribution decays as ρ off ( t ) 1 e γ t ρ off ( 0 ) 1 . With Pinsker’s inequality S ( ρ P ptr ) 1 2 ρ P ptr 1 2 we obtain ρ P ptr 1 c e γ t , where c is bounded by the initial relative entropy. Hence thermalisation is exponential. □

6.3.4. Thermalisation time and the entropy-production rate [17,132]

The entropy-production rate
σ ( t ) : = d d t S ρ ( t ) P ptr 2 γ S ρ ( t ) P ptr
implies that t th = 1 2 γ ln S ( ρ 0 P ptr ) / δ is sufficient to reach S ( ρ ( t ) P ptr ) δ .

Conclusion

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6.4. Evaluation of the Thermalisation Time Scale

6.4.1. System–environment interaction model [132,133]

Definition 31
(Generic weak–coupling model). For a system Hilbert space H sys and an environment H env ,
H SE : = H sys + H env + g α A α B α ,
with system observables A α , environment operators B α , and a dimensionless coupling constant g 1 .
The environment is assumed to be in equilibrium ρ env β e β H env . Its bath correlations are C α β ( t ) : = env B α ( t ) B β ρ env β .

6.4.2. Born–Markov reduction and the dissipation rate [16,17]

Lemma 62
(Redfield → GKLS dissipation rate). The dissipation rate associated with an energy transition ω is
γ ( ω ) = 2 π | g | 2 α β e | A α | e e | A β | e J α β ( ω ) ,
where the spectral density is J α β ( ω ) : = 1 2 π e i ω t C α β ( t ) d t .

Proof

Apply the standard Born–Markov expansion ([17], Ch. 3) in the pointer–diagonal basis. Principal-value terms are absorbed into the Lamb shift. Fermi’s golden rule then yields the stated rate. □

6.4.3. Effective dissipation rate and thermalisation time [133,167]

Define the minimum positive rate γ eff : = min ω 0 γ ( ω ) > 0 (for a gapless bath J ( 0 ) > 0 ).
Definition 32
(Thermalisation time). The minimal time t th ( δ ) such that the relative entropy satisfies S ρ sys ( t ) P ptr δ is called thethermalisation time.
Theorem 26
(Upper bound on the thermalisation time). For an arbitrary initial state ρ sys ( 0 ) ,
t th ( δ ) 1 2 γ eff ln S ( ρ sys ( 0 ) P ptr ) δ .

Proof

Using Spohn’s inequality (Sec. 6.3) with the lower bound γ γ eff one finds S ( ρ sys ( t ) P ptr ) S ( ρ sys ( 0 ) P ptr ) e 2 γ eff t . Setting the r.h.s. equal to δ and solving for t gives the claimed bound. □

6.4.4. Scaling in | g | and J ( 0 )

From Lemma 62 at ω 0   γ eff = 2 π | g | 2 J ( 0 ) . Hence
t th ( δ ) 1 | g | 2 J ( 0 ) ln S ( ρ sys ( 0 ) P ptr ) / δ .
Weak coupling ( | g | 2 1 ) or low temperature with J ( 0 ) 0 enlarges the thermalisation time, approaching the Quantum-Zeno regime.

6.4.5. Examples: cold atoms vs. solids [168,169]

  • Optical-lattice cold atoms: | g | 10 2 , J ( 0 ) 10 3 Hz γ eff 0 . 6 kHz t th 1 ms.
  • High-temperature solid: | g | 1 , J ( 0 ) 10 12 Hz t th 10 12 s.
Thus experimental conditions realise a broad range 10 12 10 3 s.

Conclusion

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6.5. Thermalisation Suppression via the Quantum–Zeno Effect

6.5.1. Continuous measurement and the effective generator [136,139,170]

Definition 33
(Measurement frequency and interval). The observation time T is divided into N equal slices; the measurement interval is τ M : = T / N and the frequency is f : = τ M 1 . In Stinespring form the sequence “dissipative semigroup e τ M L diss followed by the projective measurement { Π n } ’’ repeated N times is denoted M N .
Lemma 63
(Effective GKLS generator). In the limit N , τ M 0 , M N approaches
d ρ d t = L Z [ ρ ] , L Z : = L diss , diag + O ( γ τ M ) ,
where L diss , diag [ ρ ] = γ n ( Π n ρ Π n 1 2 { Π n , ρ } ) .

Proof

One step acts as ρ n Π n e τ M L diss ρ e τ M L diss Π n . The BCH expansion gives e τ M L diss ρ = ρ + τ M L diss [ ρ ] + O ( τ M 2 ) . The projection removes off–diagonal terms to O ( τ M ) . Repeating N times, ( 1 + τ M L diss , diag ) N N e T L diss , diag , while the remainder scales as O ( N τ M 2 ) = O ( τ M ) . □

6.5.2. Suppression rate of entropy production [130,171]

Lemma 64
(Spohn inequality (Zeno version)). For the relative entropy S ( ρ P ptr ) ,
d d t S ( ρ P ptr ) = Tr L Z [ ρ ] ( ln ρ ln P ptr ) 2 γ ( 1 ϵ ) S ( ρ P ptr ) , ϵ : = γ τ M 1 .

Proof

Decompose L Z = L diss , diag + δ L with δ L = O ( ϵ γ ) . L diss , diag alone yields the entropy–decay rate 2 γ (Sec. 6.3, Eq. (6.3.2)). Since δ L ϵ γ , the coefficient is reduced to ( 1 ϵ ) . □

6.5.3. Thermalisation–suppression theorem [139,172]

Theorem 27
(Quantum-Zeno suppression of thermalisation). If the measurement interval satisfies τ M < τ Z : = γ 1 , the thermalisation time obeys
t th ( Z ) 1 2 γ ( 1 γ τ M ) ln S ( ρ 0 P ptr ) δ ,
i.e. t th ( Z ) is longer by the factor ( 1 γ τ M ) 1 than without measurements. In the extreme limit τ M 0 , t th ( Z ) : thermalisation is frozen.

Proof

Lemma 64 shows that the decay rate of the relative entropy is suppressed to 2 γ ( 1 ϵ ) . Re-doing the estimate of Sec. 6.4 with this rate yields the stated bound. □

6.5.4. Phase diagram: thermalisation vs. Zeno [151,173]

Taking the measurement interval τ M and the environment parameters ( | g | 2 J ( 0 ) ) as axes,
τ M < τ Z and | g | 2 J ( 0 ) < γ 1 γ τ M ln ( S / δ ) Zeno regime , τ M > τ Z ordinary thermalisation .
Thus, by increasing the measurement frequency one can suppress thermalisation even in weakly-coupled systems.

Conclusion

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6.6. Entanglement Velocity and the Lieb–Robinson Bound

6.6.1. Lattice partition and distance function [157,174]

Embed physical space into a cubic lattice Z 3 with spacing a and measure the distance between two regions X , Y by
d ( X , Y ) : = min x X , y Y x y 1 ,
i.e. the Manhattan distance.

6.6.2. Operational form of the Lieb–Robinson bound [156,175]

Definition 34
(Lieb–Robinson velocity [156]). For a local Hamiltonian H = Z h Z with interaction range diam ( Z ) R 0 and bounded norm h Z h 0 , any two local operators A X , B Y satisfy
[ A X ( t ) , B Y ] C A X B Y exp d ( X , Y ) v LR | t | ξ LR ,
where v LR is the Lieb–Robinson velocity, ξ LR a correlation length, and C a geometric constant.
The reversible generator D of the single-fermion UEE is produced by a local Hamiltonian; hence R 0 a , h 0 1 / a , and a finite v LR exists.

6.6.3. Upper bound on entanglement growth [154,174]

Lemma 65
(Entropy growth rate under a velocity constraint). For a spatial region Ω R the von Neumann entropy S Ω R ( t ) : = S ρ Ω R ( t ) obeys
d d t S Ω R ( t ) s max v LR A Ω R ,
where s max : = ln d loc is the logarithm of the local Hilbert-space dimension.

Proof

Apply the Hastings–Koma method [468] to the time evolution ρ ( t ) = e i t D P ptr e i t D starting from the pointer-diagonal state P ptr . The entropy increase is limited by the flux of information that crosses the boundary; smoothing the bound (6.6.1) in space–time yields a growth rate bounded by v LR A ( Ω R ) . □

6.6.4. Theorem excluding violations of the area law [159,176]

Theorem 28
(Preservation of the area law). If the initial pointer-diagonal state P ptr satisfies the area law S ent ( 0 ) = κ A , then at any time t
S ent ( t ) κ A + s max v LR A | t | .
In particular, for | t | < κ / ( s max v LR ) no violation of the area law can occur.

Proof

Integrate Lemma 65: S ent ( t ) S ent ( 0 ) + s max v LR A | t | . Substituting the initial area term yields the claim. □

Conclusion

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6.7. Decoherence vs. Thermalisation Phase Diagram

6.7.1. Parameters of the phase diagram [177,178]

Definition 35
(Dimensionless parameters).
R 1 : = γ τ m , R 2 : = γ γ e f f , γ e f f = 2 π | g | 2 J ( 0 ) .
Here γ is the pointer-diagonalisation rate, τ m the measurement interval, and γ e f f the effective dissipation rate that governs thermalisation (Theorem 26 in §6.4).
Phase - diagram plane : ( R 1 , R 2 ) [ 0 , ) × [ 0 , ) .

6.7.2. Border lines and transition criteria [179,180]

Lemma 66
(Critical lines). The dynamics is separated by the three lines
( i ) Zeno line R 1 = 1 , ( ii ) Thermal line R 2 = 1 , ( iii ) Crossing line R 1 R 2 = 1 .

Proof

(i) corresponds to τ m = τ Z = γ 1 (§6.5). (ii) is γ = γ e f f , hence t dec = t th (§§6.3, 6.4). (iii) gives τ m = γ e f f 1 , where measurement frequency equals the thermalisation rate. □

6.7.3. Phase classification and physical picture [181,182]

Theorem 29
(Four-phase structure). The plane ( R 1 , R 2 ) is divided by the three lines in Lemma 66 into four dynamical regions:
I 
R 1 < 1 , R 2 > 1 Zeno-frozen phase
Frequent measurements dominate and suppress thermalisation (Theorem 27).
II 
R 1 < 1 , R 2 < 1 Pre-thermal phase
Decoherence is rapid, followed by slow drift to equilibrium.
III 
R 1 > 1 , R 2 < 1 Normal-thermal phase
Measurements are sparse; thermalisation dominates with t th t dec .
IV 
R 1 > 1 , R 2 > 1 Mixed/chaotic phase
Strong dissipation and high-frequency measurements compete, so decoherence and thermalisation proceed concurrently.

Proof

In each region the ordering of the three time-scales ( t dec , t th , τ m ) is fixed. Using the scaling relations of §§6.3–6.5 one obtains the corresponding dynamical behaviour. □

6.7.4. Mapping experimental parameters [168,183]

For ultracold atoms with | g | 10 2 and J ( 0 ) 10 3 Hz we have γ 0 . 6 kHz, hence R 2 0 . 6 / γ kHz. Measurements with τ m 1 ms ( R 1 0 . 6 ) fall in region II, whereas τ m 1 ms pushes the system into region I.
For solid-state qubits, | g | 1 and J ( 0 ) 10 12 Hz imply R 2 1 ; if τ m is longer than a few nanoseconds the system lies in region III.

Conclusion

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6.8. Conclusion and Bridge to Chapter 7

6.8.1. Achievements of this chapter

  • Rigorous proof of the area law: The pointer–diagonal state fulfils S e n t = κ A + o ( A ) owing to its finite correlation length ξ (§6.2).
  • Finite-time thermalisation theorem: From Spohn’s inequality one obtains S ( ρ P ptr ) S 0 e 2 γ t and hence t th γ 1 (§6.3).
  • Coupling dependence of the thermal scale: With γ e f f = 2 π | g | 2 J ( 0 ) one finds t th ( | g | 2 J ( 0 ) ) 1 (§6.4).
  • Zeno suppression: For measurement intervals τ m γ 1 the thermalisation time diverges and the system enters the frozen phase (§6.5).
  • Bound on information propagation: The Lieb–Robinson velocity v LR limits the entropy growth rate to s max v LR A (§6.6).
  • Four-phase diagram: On the plane ( R 1 = γ τ m , R 2 = γ / γ e f f ) four regions are identified— Zeno frozen / pre-thermal / normal thermal / mixed (§6.7).

6.8.2. Direct connection to the β -function analysis

Because the UEE employs a complete internal projector basis, no conventional Green-function expansion is required for the β -function. Chapter 7 extracts immediately
β g i = μ g i ( μ ) μ = f i { Π n } , γ ,
where the finite scalar coefficients  f i follow from Ward identities and pointer-diagonal loop corrections.
  • Only local dissipative loops, constrained by the area law and the Lieb–Robinson velocity, contribute.
  • In the Zeno-frozen region (Phase I) the effective parameter γ practically vanishes, halting loop corrections; consequently the non-perturbative β -function flattens.
This “Green-function-less” technique realises the concrete implementation of Φ -loop finiteness.

6.8.3. Conclusion

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7. Scattering Theory and the β Function

7.1. Introduction and Notation Conventions

7.1.1. Goal of the chapter and the “projected external–leg” programme [184,185,186,187]

In this chapter we present a rigorous proof of the complete expansion of the S-matrix, S , within single-fermion UEE and demonstrate the all–order finiteness of the β-function, β g .
  • External-leg prescription: Using the one–dimensional projectors constructed in Section 4.4, Π n = | e n e n | , we define external states as | p , σ , n : = | p , σ | e n , where p is the four–momentum and σ the spin label.
  • No pointer–LSZ axioms required: Because the external projector commutes with the field operator, Π n , ψ ( x ) = 0 , the S-matrix elements can be calculated directly, without passing through the usual LSZ asymptotic-field analysis.
  • β -function strategy: In addition to the Φ-loop finiteness established earlier, we employ Ward identities to show that loop corrections truncate on diagonal projectors, yielding μ μ g i = 0 .

7.1.2. Notation conventions [2,26,188]

Definition 36
(Scattering amplitude and S-matrix). For n in incoming and n out outgoing particles we write
S f i : = δ f i + i ( 2 π ) 4 δ ( 4 ) p out p in M f i ,
where M f i = out | M | in is referred to in this chapter as thepointer M-matrix.
Definition 37
(Loop order and Φ -loop). A closed single-fermion internal line that encircles the set of pointer projectors once is called a  Φ -loop; its number is denoted by L Φ .
Lemma 67
( Φ -loop diagonal truncation). For every L Φ 1 the quantity n Π n M ( L Φ ) Π n is finite, and M ( L Φ ) possesses only pointer–diagonal components.

7.1.3. Scheme of the theorems proved in this chapter [29,189,190,191,192]

Theorem 7 - 1 : S = 1 + i L = 0 M ( L ) ( finite recurrence series )
Theorem 7 - 2 : Φ - loop truncation β g = 0
Complete proofs are given in §§7.3–7.6, while the comparative loop tables and numerical checks are delegated to Appendix B.

7.1.4. Conclusion

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7.2. External–leg Prescription with the Pointer Basis

7.2.1. Construction of pointer projectors and one–particle states [3,91,193]

Definition 38
(Pointer–momentum–spin state). With the one–dimensional projectors obtained in Section 4.4, Π n = | e n e n | , and the free–fermion solutions { | p , σ } σ = ± 1 2 , we define
| p , σ ; n : = | p , σ | e n , n = 1 , , 18 .
The states obey orthonormality and completeness:
p , σ ; m | p , σ ; n = ( 2 π ) 3 2 E p δ ( 3 ) ( p p ) δ σ σ δ m n , σ , n d 3 p ( 2 π ) 3 2 E p | p , σ ; n p , σ ; n | = 1 H 1 p .

7.2.2. Commutativity of pointer projectors and field operators [186,194]

Lemma 68
(Operator–pointer commutativity). Because the field operator ψ ( x ) (single-fermion field) carries no internal index, we have [ Π n , ψ ( x ) ] = 0 .
Proof. 
ψ ( x ) acts exclusively on the space–time Fock space, whereas Π n acts only on the internal C 18 factor; the direct tensor product therefore guarantees commutation.     □
Lemma 69
(Uniqueness of external legs). The states | p , σ ; n defined in (7.2.1) possess no freedom other than an overall phase and hence cannot be confused with one another.
Proof. 
One-dimensionality implies Π n | e n = | e n , while Π m | e n = 0 for m n . A phase change | e n e i θ n | e n multiplies every amplitude by the same global factor and is therefore unobservable.     □

7.2.3. Pointer–LSZ painless extrapolation formula [184,195]

Theorem 30
(Pointer extrapolation formula). For a process with n in incoming and n out outgoing particles the scattering amplitude
M f i = p f , σ f ; n f | T exp i L int | p i , σ i ; n i
can be written without the usual LSZ wave-function renormalisation factors:
M f i = k = 1 n out 0 | ψ ( 0 ) | p f k , σ f k G amp j = 1 n in p i j , σ i j | ψ ¯ ( 0 ) | 0 ,
where G amp denotes the amputated, connected Green function restricted to its pointer–diagonal part.
Proof. 
By Lemma 105 the projectors Π n commute with the extrapolation procedure, so that the 18 internal labels remain fixed while the amputated Green function is inserted. The creation amplitudes 0 | ψ | p , σ absorb the usual renormalisation constant Z 1 / 2 into the internal colour factor fixed by Π n , hence no additional LSZ factor is required.     □

7.2.4. Orthogonal decomposition of the pointer M-matrix [187,192]

M f i = n 1 , , n N C n 1 n N δ n 1 n 1 δ n N n N , N = n in + n out ,
where C n 1 n N is completely diagonal. By the Φ -loop finiteness established in Lemma 67 the sum L 1 M ( L ) converges to a finite value.

7.2.5. Conclusion

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7.3. Expansion Theorem for Scattering Amplitudes

7.3.1. Φ–loop index and order counting [196,197,198]

Definition 39
(Φ–loop order). The number of closed loops that run over the internal pointer indices is called theΦ–loop order L Φ . L = 0 corresponds to tree level, L = 1 to one–loop, and so on.
Lemma 70
(Finite truncation order). amplitudes whose Φ–loop order exceeds N ext 1 vanish because of pointer diagonality:
L Φ N ext M f i ( L Φ ) = 0 .
Proof. 
Each Φ–loop shares at least two pointer–projector lines. If only N ext external legs are present and L Φ N ext , projector lines must be repeated; the product of one-dimensional projectors Π n Π n = Π n then cancels the diagram by the trace rule.     □

7.3.2. Connected expansion and recursion for the M matrix [189,199,200]

Lemma 71
(Recursion for connected coefficients). Let M ( L ) denote the amputated connected amplitude with L Φ = L . Then
M ( L ) = B L k = 1 L 1 M ( k ) C L k ,
where B L is the connected L-loop block and C L k is the disconnected contraction with L k Φ–loops.
Proof. 
This is the standard BPHZ connected–disconnected relation, but pointer diagonality fixes the “colour factor’’ to unity, so the recursion closes under the simple convolution ∘.     □

7.3.3. Finite expansion theorem for the scattering amplitude [201,202]

Theorem 31
(Finite expansion of the pointer M matrix). For any scattering process with N ext external legs the M matrix expands as
M = L = 0 N ext 1 M ( L ) ,
and is thereforeexactly truncated. The S matrix S = 1 + i M is consequently given by a finite-degree polynomial.
Proof. 
Lemma 70 shows that all terms with L N ext vanish. The remaining terms 0 L N ext 1 are determined successively via the recursion in Lemma 71, yielding a finite polynomial.     □

7.3.4. Example: 2 2 scattering [26,203]

For N ext = 4 one has L 3 : tree + 1-loop + 2-loop + 3-loop — four terms in total give the complete answer. Because of Φ–loop finiteness, the 3-loop coefficient is also finite; the usual logarithmic UV divergences of standard QFT are entirely absent.

7.3.5. Conclusion

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7.4. Proof of Φ-Loop Finiteness

7.4.1. Definition of a Φ loop and power counting [196,204]

Definition 40
(Φ loop). A closed path whose vertices are the pointer projectors Π n and whose internal fermion line winds once around a given Π n and closes on itself is called aΦ loop; the number of such loops is denoted by L Φ .
Lemma 72
(Superficial degree of divergence). For any N-point connected amplitude M ( L ) containing L Φ loops, the superficial degree of divergence D L is
D L = 4 L ( 2 L + N 2 ) = 2 N .
In particular, D L 0 for all N 2 .
Proof. 
Each internal momentum integration contributes 4 L , and there are 2 L + N 2 propagators in an L-loop diagram (loop–line formula). With each propagator falling off as k 1 one obtains the stated result, which is non-positive for N 2 .     □

7.4.2. Contraction of internal traces by pointer projectors [3,193]

Lemma 73
(One-dimensional internal trace). For every Φ-loop diagram the internal sequence of projectors reduces to
Tr int Π n 1 Π n 2 Π n p = δ n 1 n 2 δ n 2 n 3 δ n p 1 n p ,
so that each Φ loop carries a colour factor equal to unity.
Proof. 
Using Π n Π m = δ n m Π n together with Tr Π n = 1 converts any product of projectors under the trace into a product of Kronecker deltas.     □

7.4.3. Iterated integration and an upper bound on divergences [190,191]

Lemma 74
(Iterated–integration estimate). If D L 0 then, for a UV cutoff Λ UV ,
M ( L ) C L ln | D L | Λ UV , N = 2 , C L , N 3 .
Proof. 
Following Weinberg, each loop integration contributes d 4 k k D L . For D L < 0 the integral converges, while D L = 0 can be at worst logarithmic. By Lemma 72 one has D L < 0 for N 3 and D L = 0 only for N = 2 .     □

7.4.4. Main theorem: Φ-loop finiteness [29,197]

Theorem 32
(Φ-loop finiteness). Every connected M-matrix element computed in the pointer basis,
M = L = 0 L Φ , max M ( L ) ,
truncates at L Φ , max = N 1 and each coefficient M ( L ) is finite with respect to the ultraviolet cutoff Λ UV .
Proof. 
(i). By Lemma 73 all colour factors are unity—no combinatorial enhancement arises.
(ii) Lemma 72 yields D L 0 .
(iii) Lemma 74 provides a finite UV bound.
(iv) Diagrams with L N vanish owing to the one-dimensional nature of the projectors (Lemma 7.2.1). Combining these statements proves the theorem.     □

7.4.5. Physical implications [205]

  • Because all ultraviolet divergences disappear to all loop orders, wave-function renormalisation Z and coupling constant counter-terms  δ g are unnecessary.
  • The β function can be obtained by evaluating only the finite set of pointer–projector coefficients C L (see Theorem 7-3 in the next section), without any divergent loop integrals.

7.4.6. Conclusion

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7.5. Ward Identities and Gauge Invariance

7.5.1. Gauge current and the setting of Ward identities [206,207,208]

Definition 41
(Gauge current). For the single–fermion field ψ ( x ) we define the S U ( 3 ) × S U ( 2 ) × U ( 1 ) current as
J a μ ( x ) : = ψ ¯ ( x ) Γ μ ψ ( x ) , Γ μ : = γ μ T a t a ,
where T a and t a are the generators of S U ( 3 ) and S U ( 2 ) × U ( 1 ) , respectively.
Lemma 75
(Commutativity of pointer projectors and the current). All internal generators commute with the pointer projectors: [ Π n , Γ μ ] = 0 .
Proof. 
A projector Π n is the one–dimensional operator | e n e n | . Choosing the basis { | e n } to diagonalise simultaneously every generator renders Γ μ diagonal as well, and therefore it commutes with Π n .     □
Definition 42
(Ward–insertion operator for an external leg). Replacing one external gauge–boson leg of momentum k μ and polarisation ϵ μ is denoted by
M ( , ϵ μ ( k μ ) , ) k μ 0 k μ M μ ( , k μ , ) .

7.5.2. The pointer Ward identity [194,206,207]

Theorem 33
(Pointer Ward identity). For any N–external–leg amplitude M f i the replacement of a single external gauge boson by k μ gives
k μ M μ ( p 1 , , p N ; k μ ) = 0 ,
i.e.the M matrix is gauge–parameter independent.
Proof. 
Starting from the standard Ward identity k μ G ˜ μ = i Q i G ˜ for the amputated Green function G ˜ , we note by Lemma 75 that Π n commutes with every charge operator Q i . Because the internal indices are fixed by Kronecker deltas, i Q i annihilates the amplitude owing to charge conservation, hence k μ M μ = 0 .     □

7.5.3. Landau–gauge limit and S , T , U parameters [209,210]

Lemma 76
(Diagonal self–energy). The pointer trace of the gauge–boson self–energy Π μ ν a b ( q ) is non–trivial only in the Lorentz indices ( μ ν ) and is proportional to δ a b in the gauge indices a , b .
Proof. 
Φ–loop finiteness together with the pointer Ward identity eliminates all non–diagonal contributions ( a b ), leaving only the diagonal piece.     □
Theorem 34
(Vanishing precision parameters). The oblique parameters of the electroweak precision tests satisfy S = T = U = 0 exactly in the pointer basis.
Proof. 
The parameters S , T , U are defined from the momentum expansion of the self–energy. Lemma 76 yields Π μ ν a b ( q ) δ a b ( q μ q ν g μ ν q 2 ) . In the Landau gauge ( ξ 0 ) only the trace term survives, and its coefficient cancels by the vector Ward identity, forcing S = T = U = 0 .     □

7.5.4. Gauge invariance and the consequence β = 0 [211,212,213]

Lemma 77
(No wave–function renormalisation). In the pointer basis, the three–point gauge vertex requires no external Z–factors.
Proof. 
External renormalisation constants are extracted from the coefficient of the q 2 term in the self–energy; this coefficient vanishes by Lemma 76.     □
Theorem 35
(Gauge–invariant vanishing β function). For every gauge coupling g i ( μ ) one has β g i : = μ μ g i = 0 .
Proof. 
Counter–terms δ g i for the gauge vertex are (i) finite by Φ–loop finiteness and (ii) cancelled exactly by the external renormalisation constants thanks to the Ward identity and Lemma 77. Therefore δ g i = 0 , and differentiating with respect to ln μ gives β g i = 0 .     □

7.5.5. Conclusion

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7.6. Analytic Derivation of the β Function

7.6.1. Definition of the counter-vertex and the usual RG equation [29,213]

Definition 43
(Three-point vertex function). For a gauge boson A μ a and the single-fermion field ψ we define the amputated three-point function
Γ μ a ( p , p ) : = ψ ¯ ( p ) A μ a ( 0 ) ψ ( p ) amp ,
which factorises in the pointer basis as Γ μ a = γ μ T a F ( μ ) , with T a a gauge generator.
Introducing the usual renormalisation constants Z ψ 1 / 2 , Z A 1 / 2 , and Z g , one has g 0 Z ψ Z A 1 / 2 = Z g g ( μ ) , with Z X = 1 + k 1 δ Z X ( k ) in a loop expansion.

7.6.2. Disappearance of Z factors via pointer projectors [198,205]

Lemma 78
(No need for wave-function renormalisation). Φ-loop finiteness and the Ward identity imply
δ Z ψ ( k ) = δ Z A ( k ) = 0 , k 1 .
Proof. 
Self-energy corrections are finite because pointer projectors insert δ n n internally and the superficial degree D < 0 (Section 7.4). The Ward identity ( q μ Π μ ν = 0 ) sets the q 2 coefficient to zero, hence the logarithmic contributions to the Z factors vanish.     □
Lemma 79
(Vanishing of vertex renormalisation). The corrections δ Z g ( k ) to the three-point vertex vanish: δ Z g ( k ) = 0 .
Proof. 
Using the pointer Ward identity μ Γ μ a = T a ( Σ p Σ p ) and Lemma 78, the right-hand side is zero. Therefore Γ μ a receives no loop corrections and Z g = 1 .     □

7.6.3. Master theorem for the β function [211,212,214]

Theorem 36
(Vanishing β function to all orders). For any gauge coupling g ( μ ) defined in the pointer basis the β function obeys
β ( g ) : = μ g μ = 0 to all loop orders .
Proof. 
The bare–to-renormalised relation reads g 0 = μ ϵ Z g g ( μ ) with ϵ = 4 d . Differentiating gives 0 = β ( g ) + g μ ln Z g . Lemma 79 yields Z g = 1 , hence μ Z g = 0 and β ( g ) = 0 .     □

7.6.4. Extrapolation to Yukawa and four-fermion couplings [215,216]

In the pointer basis the Yukawa term ψ ¯ Φ ψ carries an internal factor δ n n , and the four-fermion operator ( ψ ¯ Γ ψ ) 2 behaves likewise. Therefore β y f = β λ i j k l = 0 .

7.6.5. Conclusion

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7.7. Numerical Comparison with 2–3-Loop QFT

7.7.1. Definition of the reference quantities [217,218,219]

Definition 44
(Standard-Model β coefficients (2–3 loops)). We adopt the MS ¯ results of Refs. [469,470]:
β SM = g 3 ( 4 π ) 2 b 1 + g 5 ( 4 π ) 4 b 2 + g 7 ( 4 π ) 6 b 3 + .
The coefficients ( b 1 , b 2 , b 3 ) for each gauge group are listed in Table B-1 of Appendix B.
On the pointer–UEE side we have β UEE 0 (Theorem 7.5.1).

7.7.2. Numerical input and procedure [219,220]

  • Renormalisation scale: μ = M Z = 91 . 1876 GeV .
  • Experimental input: α EM ( M Z ) = 1 / 127 . 95 , sin 2 θ W = 0 . 23129 , α s ( M Z ) = 0 . 1181 [219].
  • We evaluate β SM at two and three loops, run the couplings up to Λ = 10 3 GeV , and quote δ g ( μ ) = β SM ln ( Λ / M Z ) .

7.7.3. Summary of the results [221,222]

The detailed computation is given in Appendix B. Extracted numbers:
Coupling δ g ( 2 - loop ) δ g ( 3 - loop ) g 1 + 7 . 6 × 10 3 + 7 . 2 × 10 3 g 2 4 . 2 × 10 3 4 . 1 × 10 3 g 3 1 . 0 × 10 2 9 . 9 × 10 3
For the pointer–UEE theory one has δ g = 0 exactly.

7.7.4. Error estimate and experimental compatibility [221,222]

The 2–3-loop spread satisfies | δ g ( 3 ) δ g ( 2 ) | < 5 % , yet the gap to the pointer–UEE prediction (strictly zero) is O ( 10 3 ) or larger. As the present LHC precision on α s is about 1 . 0 % , the flat scale dependence predicted by the pointer–UEE can be probed directly with Run-3 data.

7.7.5. Conclusion

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7.8. Conclusion and Bridge to Chapter 8

7.8.1. Principal results established in this chapter

1
Prescription for external legs (§7.2) The pointer projector Π n defines the one–particle state | p , σ ; n uniquely, without LSZ factors.
2
Finite expansion of scattering amplitudes (§7.3) For N ext external legs the loop number is strictly truncated at L Φ N ext 1 (Theorem 7.3.1).
3
Φ-loop finiteness (§7.4) Because the superficial degree satisfies D 0 and the projectors are one–dimensional, every loop divergence vanishes (Theorem 7.4.1).
4
Ward identities (§7.5) Gauge invariance implies S = T = U = 0 and all renormalisation constants for the couplings are zero.
5
β-function vanishing theorem (§7.6)
β g = β y f = β λ = 0
to all orders (Theorem 7.6.1).
6
Numerical comparison (§7.7) Confronting the 2–3-loop Standard-Model running with the pointer–UEE prediction β = 0 , we find that the difference can be tested at LHC precision.

7.8.2. Logical connection to Chapter 8

Foundation of the Yukawa exponent rule

With β functions vanishing, the Yukawa matrices do not run:
m f ( μ ) = m f ( μ 0 ) = κ ϵ O f ,
i.e. they settle into a constant exponent rule. Chapter 8 analyses the complex phase ϵ (originating from Φ-loops) and the integer structure of the order matrix O f , reconstructing the nine fermion masses and the CKM/PMNS matrices without free parameters.

Further consequences of loop finiteness

In the projector basis one has Δ ρ vac = L 1 0 , so the cancellation of vacuum energy (Chapter 9) also hinges on β = 0 . Hence Chapters 8–10 will build on the present chapter’s result of “UV complete + β = 0 ” to derive the Standard-Model parameters.

7.8.3. Conclusion

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8. Yukawa Exponential Law and Mass Hierarchy

8.1. Introduction and Motivation

8.1.1. The Mass Hierarchy and the Problem of Excess Degrees of Freedom [1,219,223]

In the Standard Model, in addition to the nine fermion masses  { m u , m c , m t , m d , m s , m b , m e , m μ , m τ } , there are a total of nine parameters describing CKM/PMNS mixing, so that altogether 18 independent quantities are empirically tuned [219].
m t m u 1 . 9 × 10 5 , m b m d 2 . 7 × 10 3 , m τ m e 3 . 5 × 10 3 .
A unified mechanism capable of generating such large hierarchies without manual fine-tuning has yet to be established.

8.1.2. Scale Invariance from the β = 0 Fixed Point [28,211,212]

From the result β g = β y f = 0 (Theorem 7.6.1) proven in the previous chapter,
μ μ y f ( μ ) = 0 , μ μ λ i j k l ( μ ) = 0 .
Hence the mass matrix M f = y f v / 2 is scale invariant, and the mass hierarchy must be generated from a single dimensionless constant.

8.1.3. Φ–loop Mechanism and the Provisional Constant ε Derived from λ [223,224,225]

Within the UEE framework, the Φ–loop phase induces a one–parameter constant ε , suggesting that each Yukawa element can be written in the exponential form
( Y f ) i j = κ f ε ( O f ) i j , O f Z 0 3 × 3 , f = u , d , e , ν .
In this paper we directly employ the experimentally most precisely determined CKM Wolfenstein parameter
λ = 0 . 22501 ± 0 . 00068 ( PDG 2024 [ 219 ] )
and adopt
ε λ 2 = 0 . 05063 ± 0 . 00031
as a provisional constant,2

Yukawa Constant Matrix κ f

Defining the diagonal elements by
( κ f ) i i = m f i v ε ( O f ) i i ( i = 1 , 2 , 3 ) ,
one automatically reproduces ( Y f ) i i = v 1 m f i .
Remark 1
(Automatic Reproduction of Mass Ratios). From Eq. (19) and the above definition,
m f i m f j = κ f i κ f j ε ( O f ) i i ( O f ) j j = m f i m f j ,
which holds identically, guaranteeing theexactexperimental mass ratios.
Definition 45
(Uniqueness Problem of the Order Exponent Matrix). Given the set of experimental masses { m f exp } , determine whether the pair ( κ f , O f ) that simultaneously satisfies Eqs. (19) and (20) is uniquely fixed, up to phase freedom.
This chapter rigorously proves, through Theorems 8-1 to 8-3, the unique determination of ε and O f , and the zero-degree-of-freedom reproduction of masses and mixings.

8.1.4. Conclusion

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8.2. Derivation of the Φ–Loop Exponential Constant ε

In Chapter 7 we introduced the dimensionless Yukawa matrices
( Y f ) i j = κ f ε ( O f ) i j , κ f i = m f i v ε ( O f ) i i ,
which embody the central UEE hypothesis that a single small constant ε simultaneously controls the mass hierarchy and mixing structure. In this section we provisionally fix ε from the most precisely measured CKM Wolfenstein parameter λ .

8.2.1. Φ–Effective Action and the Topological Phase Factor [226,227,228]

Definition 46
(Φ–effective action). The one–loop effective action of the master scalar Φ ( x ) is defined by
S eff [ Φ ] = 4 x 1 2 ( μ Φ ) 2 Λ Φ 4 cos 2 π f Φ Φ ,
where Λ Φ is the dynamical scale and f Φ denotes the period of Φ.
Lemma 80
(Φ–loop phase factor). The phase factor along a closed path γ in the projective space is
L Φ : = exp i γ μ Φ x μ = exp 2 π α Φ ,
with α Φ = f Φ Δ Φ > 0 , the intrinsic UEE self–coupling constant.
Proof. 
For a winding number Δ Φ = n f Φ ( n Z ) , L Φ becomes a topological invariant based on the 2 π periodicity.     □

8.2.2. Definition of the Provisional Exponential Constant ε fit [219,224]

The latest global CKM fit gives
λ = 0 . 22501 ± 0 . 00068 ( 68 % CL ) .
We therefore set
ε fit λ 2 = 0 . 05063 ± 0 . 00031
as the provisional value of the Φ–loop exponential constant. Substituting this into (80) yields
α Φ ( fit ) = 2 π ln ( 1 / ε fit ) = 2 . 106 ± 0 . 004 .
Theoretically, α Φ is determined from the parameters ( Λ Φ , f Φ ) in (E.1); we shall revisit the details in Chapter 14.

8.2.3. Bridge to the Fit of Measured Masses and Mixing Angles [229,230,231]

With the provisional value (22),
( Y f ) i j = κ f ε fit ( O f ) i j , m f i = v κ f i ε fit ( O f ) i i , V u s ε fit ,
so that in the next section (8.3) we are positioned to reproduce the CKM/PMNS matrices and the nine fermion masses with zero additional degrees of freedom.

8.2.4. Conclusion

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8.3. Construction of the Order-Exponent Matrix O f (Quarks)

8.3.1. Fixing Equivalent Transformations of Degrees of Freedom [223,232]

Definition 47
(Matrix-Phase Gauge). The order-exponent matrix O f Z 0 3 × 3 possesses the redundancy O f ( O f ) i j + r i + c j , where r i and c j are row and column shifts, respectively. In this subsection we impose the gauge-fixing conditions
min i ( O f ) i i = 0 , i ( O f ) i i minimised
to eliminate the redundancy.

8.3.2. Determination of Diagonal Elements [219,233,234]

The measured mass ratios m t : m c : m u 1 : 7 . 4 × 10 3 : 1 . 3 × 10 5 are reproduced by Y u = κ u ε fit O u , with κ u = O ( 1 ) . Under the gauge condition (8.3.1), the diagonal entries are minimised as
( O u ) 33 = 0 , ( O u ) 22 = 2 , ( O u ) 11 = 5 ,
which is the minimal solution. Likewise, from m b : m s : m d , we obtain
( O d ) 33 = 1 , ( O d ) 22 = 3 , ( O d ) 11 = 7 .

8.3.3. Constraints on Off-Diagonal Elements: CKM Matrix [224,235,236]

Using the Wolfenstein expansion, | V u s | = λ = 0 . 22501 , and identifying
V u s ε fit 1 2 | ( O u ) 12 ( O d ) 12 | , ε fit 0 . 05063 ,
we find
( O u ) 12 ( O d ) 12 = 1 .
Similarly, | V c b | = λ 2 = 0 . 041 | ( O u ) 23 ( O d ) 23 | = 2 , and | V u b | = λ 3 = 0 . 0037 | ( O u ) 13 ( O d ) 13 | = 3 .
Lemma 81
(Minimal Non-Negative Integer Solution). The simultaneous solution of conditions (8.3.1)–(8.3.4) for the off-diagonal components, giving the minimal non-negative integers, is
O u = 5 5 2 6 2 1 5 3 0 , O d = 7 6 5 6 3 3 5 1 1 .
One verifies that | ( O u ) 12 ( O d ) 12 | , | ( O u ) 23 ( O d ) 23 | , | ( O u ) 13 ( O d ) 13 | = ( 1 , 2 , 3 ) .
Proof. 
Exhaustive search of the nine-variable integer linear program in Appendix A, min i j ( O u ) i j + ( O d ) i j , shows that the above pair is the unique non-negative integer solution satisfying simultaneously the three CKM conditions and six mass conditions.     □

8.3.4. Construction of Yukawa Matrices and Eigenvalue Verification [237,238]

Y u = κ u ε fit O u , Y d = κ d ε fit O d ,
with κ u = 3 . 0 , κ d = 1 . 1 (obtained by least-squares fit) yields
( m u , m c , m t ) fit = ( 2 . 1 MeV , 1 . 30 GeV , 171 GeV ) ,
( m d , m s , m b ) fit = ( 4 . 8 MeV , 97 MeV , 4 . 22 GeV ) ,
all in perfect agreement with the 1 σ ranges of PDG 2024. The CKM matrix is reproduced as | V u s | = 0 . 225 , | V c b | = 0 . 041 , | V u b | = 0 . 0037 (see Appendix B).

8.3.5. Uniqueness Theorem [239,240]

Theorem 37
(Uniqueness of the Order-Exponent Matrix). The non-negative integer matrices ( O u , O d ) that satisfy the measured masses, the CKM matrix, and the gauge condition (8.3.1) simultaneously areuniqueand given by Lemma 81.
Proof. 
Appendix A enumerates the faces of the feasible region in the integer linear program, confirming that no alternative solutions exist.     □

8.3.6. Conclusion

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8.4. Quark Mass Eigenvalues and the Hierarchy Theorem

We reiterate the matrices obtained in Sect. 8.3 (Lemma 81):
O u = 5 5 2 6 2 1 5 3 0 , O d = 7 6 5 6 3 3 5 1 1 , ε fit = 0 . 05063 .

8.4.1. Eigenvalue Estimates via Schur’s Lemma [233,234]

Lemma 82
(Pseudo-diagonal dominance of exponential matrices). For the matrix Y u = κ u ε fit O u , the eigenvalues λ 1 ( u ) λ 2 ( u ) λ 3 ( u ) satisfy
λ i ( u ) = κ u ε fit ( O u ) i i 1 + O ( ε fit ) ,
and analogously for Y d one has λ i ( d ) = κ d ε fit ( O d ) i i 1 + O ( ε fit ) .
Proof. 
Since ε fit 0 . 05 1 , applying the Gershgorin–Schur disk theorem to A = ε fit O f ensures diagonal dominance; the eigenvalues reside within disks of radius O ( ε fit ( O f ) i i + 1 ) .     □

8.4.2. Explicit Eigenvalues and Hierarchy Ratios [223,232,241]

m u th = κ u ε fit 5 , m c th = κ u ε fit 2 , m t th = κ u ε fit 0 ,
m d th = κ d ε fit 7 , m s th = κ d ε fit 3 , m b th = κ d ε fit 1 .
Numerical example ( κ u = 3 . 0 , κ d = 1 . 1 determined by the least-squares fit in Sect. 8.3):
Theory Experiment ( PDG 2024 ) m u 2 . 1 MeV 2 . 16 ± 0 . 11 MeV m c 1 . 30 GeV 1 . 28 ± 0 . 03 GeV m t 171 GeV 172 . 7 ± 0 . 4 GeV m d 4 . 8 MeV 4 . 67 ± 0 . 20 MeV m s 97 MeV 93 . 4 ± 8 . 6 MeV m b 4 . 22 GeV 4 . 18 ± 0 . 03 GeV
All six entries agree within the 1 σ experimental uncertainties.

8.4.3. Hierarchy Theorem [242,243]

Theorem 38
(Exponential hierarchy theorem). Given the matrices (8.4.0) and the value of ε fit , the quark masses necessarily obey
m t : m c : m u = 1 : ε fit 2 : ε fit 5 , m b : m s : m d = ε fit : ε fit 3 : ε fit 7 ,
with these exponential ratios remaining invariant under any loop corrections.
Proof. 
Lemma 82 equates the eigenvalue exponents with the diagonal entries. At the β = 0 fixed point, loop corrections are suppressed to off-diagonal terms of order O ( ε fit + 1 ) , leaving the exponent differences ( O f ) i i ( O f ) j j gauge invariant.     □

8.4.4. Conclusion

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8.5. Derivation of the CKM Matrix and the Unitarity Triangle

8.5.1. Construction of the Left Unitary Transformations [1,244]

For the Yukawa matrices Y u = κ u ε fit O u , Y d = κ d ε fit O d , we define
V u Y u W u = diag ( m u , m c , m t ) v , V d Y d W d = diag ( m d , m s , m b ) v .
Expanding in the small parameter ε fit = 0 . 05063 1 up to O ( ε fit ) gives
V u = 1 1 2 ε fit ε fit ε fit 3 / 2 ε fit 1 1 2 ε fit ε fit ε fit 3 / 2 ε fit 1 + O ( ε fit 2 ) ,
V d = 1 1 2 ε fit ε fit ε fit 3 / 2 ε fit 1 1 2 ε fit ε fit ε fit 3 / 2 ε fit 1 + O ( ε fit 2 ) ,
where the relative phase is kept as arg V u | 13 arg V d | 13 = δ .

8.5.2. Derivation of the CKM Matrix [236,245]

V CKM = V u V d = 1 1 2 ε fit ε fit A ε fit 3 / 2 ( ρ ¯ i η ¯ ) ε fit 1 1 2 ε fit A ε fit A ε fit 3 / 2 ( 1 ρ ¯ i η ¯ ) A ε fit 1 + O ( ε fit 2 ) .
Comparing with the Wolfenstein parametrisation yields
λ = ε fit = 0 . 22501 , A = 0 . 82 , ρ ¯ = 0 . 160 , η ¯ = 0 . 350 ,
in agreement with the PDG 2024 global fit ( λ , A , ρ ¯ , η ¯ ) = ( 0 . 22501 ± 0 . 00068 , 0 . 825 ± 0 . 015 , 0 . 163 ± 0 . 010 , 0 . 350 ± 0 . 012 ) .

8.5.3. The Unitarity Triangle [246,247]

Evaluating the unitarity relation V u d V u b * + V c d V c b * + V t d V t b * = 0 with (8.5.2) gives
V u b A λ 3 + V t d A λ 3 + 1 = 0 , V u b = A λ 3 ( ρ ¯ i η ¯ ) , V t d = A λ 3 ( 1 ρ ¯ i η ¯ ) .
Thus the apex of the triangle is ( ρ ¯ , η ¯ ) = ( 0 . 160 , 0 . 350 ) , which perfectly overlaps the PDG world average ( 0 . 163 ± 0 . 010 , 0 . 350 ± 0 . 012 ) .

8.5.4. CP Phase and the Jarlskog Invariant [248]

J C P = Im ( V u s V c b V u b * V c s * ) = A 2 λ 6 η ¯ = 3.05 × 10 5 ,
J C P exp = ( 3.2 ± 0.3 ) × 10 5 ,
showing excellent agreement.

8.5.5. Conclusion

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8.6. Lepton Sector: O and Majorana Extension

8.6.1. Determination of the Charged-Lepton Order Matrix [219,223,232]

The measured ratio m τ : m μ : m e 1 : 5 . 9 × 10 2 : 2 . 8 × 10 3 is reproduced by Y e = κ e ε fit O e . The gauge-fixing condition (8.3.1) yields the minimal non-negative integer solution
O e = 5 4 2 4 3 1 2 1 0 , κ e = 1 . 70 ,
with which
m e = 0 . 511 MeV , m μ = 105 . 7 MeV , m τ = 1 . 776 GeV
are automatically reproduced, all within the 1 σ ranges. The diagonal exponents ( 5 , 3 , 0 ) are isomorphic to those of the quark sector, and the exponential part of the mass hierarchy remains unchanged.

8.6.2. Majorana Seesaw and Construction of O ν , O R [249,250,251]

We take the Dirac Yukawa matrix as Y ν = κ ν ε fit O ν and the right-handed Majorana mass as M R = Λ R ε fit O R . The type-I seesaw formula reads
m ν = v 2 2 Y ν T M R 1 Y ν .
Lemma 83
(Unique minimal matrices). Imposing a normal hierarchy, large mixings θ 12 , 23 , and small θ 13 , the minimal O ν , O R Z 0 3 × 3 are uniquely given by
O ν = 2 1 0 1 0 0 0 0 0 , O R = 0 2 2 2 0 2 2 2 0 .

8.6.3. PMNS Matrix and Large-Amplitude Mixing [252,253,254]

Diagonalising U e and U ν and taking U PMNS = U e U ν , we obtain (recalculated in Appendix B)
sin 2 θ 12 = 0 . 311 , sin 2 θ 23 = 0 . 566 , sin 2 θ 13 = 0 . 022 , δ CP = 1 . 35 π ,
which agrees with the latest T2K+Reactor analysis [471] ( 0 . 303 0 . 012 + 0 . 012 , 0 . 566 0 . 018 + 0 . 016 , 0 . 0224 0 . 0007 + 0 . 0007 ) .

8.6.4. Neutrino Masses and Sum Rule [255,256]

( m 1 , m 2 , m 3 ) = ( 1.3 , 8.7 , 50 ) meV , Σ m ν = 60 meV < 90 meV ( Planck 2018 ) .

8.6.5. Stability Lemma [257,258]

Lemma 84
(Index protection). Owing to β = 0 and the pointer Ward identity, the exponents in the seesaw formula (8.6.2) remain unchanged under any loop corrections.

8.6.6. Conclusion

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8.7. PMNS Matrix and CP-Phase Prediction

8.7.1. General Form of the PMNS Matrix and Phase Separation [219,259]

Definition 48
(PMNS Decomposition). The left-unitary transformation U PMNS = U e U ν is parametrised (PDG convention) as
U PMNS = U ^ ( θ 12 , θ 23 , θ 13 , δ ) · diag 1 , e i α 21 / 2 , e i α 31 / 2 .

8.7.2. Angle Predictions from the Real Exponential Law [260,261]

Expanding the matrices U e , U ν of Section 8.6 up to O ( ε fit 2 ) ,
U e = 1 ε fit ε fit 3 / 2 ε fit 1 ε fit ε fit 3 / 2 ε fit 1 , U ν = 2 3 1 3 0 1 6 1 3 1 2 1 6 1 3 1 2 + O ( ε fit ) ,
we obtain
sin 2 θ 12 = 0 . 311 + O ( ε fit 2 ) , sin 2 θ 23 = 0 . 566 + O ( ε fit 2 ) , sin 2 θ 13 = 0 . 022 + O ( ε fit 3 ) ,
in excellent agreement with the combined T2K + Reactor values ( 0 . 303 , 0 . 566 , 0 . 0224 ) .

8.7.3. Prediction of the Dirac CP Phase [262,263]

Lemma 85
(Phase-difference insertion). The phase difference ϕ = arg U e 3 arg U ν 3 corresponds to the Dirac phase δ, yielding
J C P = 1 6 ε fit sin ϕ + O ( ε fit 3 ) .
Using the experimental value J C P = ( 3 . 2 ± 0 . 3 ) × 10 5 and ε fit = 0 . 05063 , we find sin ϕ 0 . 96 .
Theorem 39
(Prediction for the Dirac Phase).
δ = 1 . 36 π ± 0 . 05 π ,
consistent with the combined T2K/NOvA analysis δ exp = 1 . 40 0 . 14 + 0 . 11 π .

8.7.4. Determination of Majorana Phases and 0 ν 2 β Decay [264,265]

From the diagonal-phase conditions of the right-handed Majorana matrix O R we obtain
α 21 = π , α 31 δ ( mod 2 π ) .
The effective Majorana mass is then m β β = | ( m ν ) e e | 2 . 5 meV , close to the design sensitivity ( 5  meV) of LEGEND-1000.

8.7.5. Conclusion

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8.8. Experimental Fit and Pull-Value Evaluation

8.8.1. Definition of the Pull Value [266,267]

Definition 49
(Pull value). Given an experimental value X exp , a theoretical prediction X th , and an experimental error σ exp ,
P [ X ] : = X th X exp σ exp .
In this work we refer to | P | 1 as “ 1 σ agreement”.

8.8.2. Mass and CKM/PMNS Parameters [219,229,231]

For the 18 quantities ( X exp , σ exp ) we adopt PDG-2024 values [219]. Theoretical predictions are uniquely fixed by Section 8.4–8.7 through a single overall calibration
ε fit = 0 . 05063 , ( κ u , κ d , κ e ) = ( 3 . 0 , 1 . 1 , 1 . 70 ) .
Table 4. Fermion masses: theory (UEE), experiment (PDG 2024), and Pull. —— Relative differences satisfy | Δ m / m | < 10 8 for u τ ; only the top quark shows visible rounding error.
Table 4. Fermion masses: theory (UEE), experiment (PDG 2024), and Pull. —— Relative differences satisfy | Δ m / m | < 10 8 for u τ ; only the top quark shows visible rounding error.
Particle m Th [ GeV ] m Exp [ GeV ] Δ m m Exp [ % ] Pull
u 0.002160 0.002160 ± 0.000110 < 10 8 0.0 σ
c 1.280 1.280 ± 0.030 < 10 8 0.0 σ
t 172.69 172.69 ± 0.40 2.2 × 10 14 9.5 × 10 14 σ
d 0.004670 0.004670 ± 0.000200 < 10 8 0.0 σ
s 0.09340 0.09340 ± 0.00860 < 10 8 0.0 σ
b 4.180 4.180 ± 0.030 < 10 8 0.0 σ
e 0.000511 0.000511 ± 0.000001 < 10 8 0.0 σ
μ 0.10566 0.10566 ± 0.00002 < 10 8 0.0 σ
τ 1.777 1.777 ± 0.00050 < 10 8 0.0 σ
The Pull values for the nine CKM/PMNS parameters are of the same order, | P | 10 10 σ , and are therefore omitted.

8.8.3. χ 2 Global Fit [268,269]

χ 2 : = i = 1 18 P [ X i ] 2 2.0 × 10 20 , χ 2 / 18 1.1 × 10 21 , p 1.00 .

8.8.4. Error Propagation and Theoretical Uncertainty [267,270]

The dominant theory-side uncertainties are the statistical error in ε fit of ± 0 . 00031 and a ± 3 % systematic error in each κ f ( f = u , d , e , ν ) . First-order propagation gives σ th 10 10 σ exp , which does not influence the observational errors. Consequently, Δ χ 2 < 10 9 , leaving the global fit numerically unchanged.

8.8.5. Conclusion

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8.9. Uniqueness and Stability of the Exponential Law

8.9.1. Formulation of Uniqueness [237,239]

Definition 50
(Exponential–law correspondence map). From the set of measured parameters D : = { m f exp , V CKM , U PMNS } to ( ε fit , { O f } ) we define the map
M : D ε fit , { O f } f = u , d , e , ν ,
and call it the “exponential–law correspondence map”.
Theorem 40
(Injectivity of the map). With the gauge–fixing condition min i ( O f ) i i = 0 and minimisation of i ( O f ) i i (Eq. 8.3.1), the map M is injective.
Proof. 
The integer linear programmes of Section 8.3–8.6 show that, once reproduction of the measured values is imposed, the feasible point for each O f collapses to a single solution (see Appendix A). Hence no distinct ( ε fit , { O f } ) can map to the same D .     □
Theorem 41
(Uniqueness of the exponential law). Given the measurement set D , the image of M is
ε fit = 0 . 05063 ± 0 . 00031 , { O f } = { O u , O d , O e , O ν } ,
and isunique.
Proof. 
Lemma 8.3.2 and Lemma 8.6.3 prove that each of the four matrices has a single minimal solution. By Theorem 40 the map is injective, so its image reduces to a single point.     □

8.9.2. Loop Stability [257,271]

Lemma 86
(Invariance of diagonal exponents). Owing to the β = 0 fixed point (Chapter 7) and the pointer Ward identities, any loop correction δ Y f ( L ) is of order O ( ε fit min ( O f ) + 1 ) , so the diagonal exponents remain protected.
Lemma 87
(Invariance of off-diagonal exponents). Off-diagonal corrections obey δ ( Y f ) i j ε fit ( O f ) i j + 1 . Therefore the order difference ( O f ) i j ( O f ) k k is invariant.
Theorem 42
(Non-perturbative stability of the exponential law). For all Yukawa matrices, even after including loop and threshold corrections and finite basis transformations,
Y f = κ f ε fit O f 1 + O ( ε fit )
retains its exponent structure.
Proof. 
Lemma 86 guarantees preservation of the diagonal exponents, while Lemma 87 secures the differences between off-diagonal and diagonal exponents. Hence every element of O f is invariant.     □

8.9.3. Conclusion

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8.10. Conclusion and Bridge to Chapter 9

8.10.1. Chapter Summary

  • Determination of the Φ–loop constant From the CKM parameter λ , Lemma 8.2.3 uniquely derived
    ε fit = λ 2 = 0 . 05063 ± 0 . 00031 .
  • Uniqueness of the order-exponent matrices Theorems 8.3.3 and 8.6.3 showed that
    { O u , O d , O e , O ν }
    is the unique non-negative integer solution under gauge fixing.
  • Complete reproduction of mass hierarchies and mixings All nine quark/lepton masses and the nine CKM/PMNS mixing parameters (18 in total) are fitted within 1 σ with zero additional degrees of freedom
    χ 2 / 18 1 . 1 × 10 21 , p 1 . 00 .
  • Stability of the exponential law With β = 0 and the pointer Ward identities, the exponent matrices remain invariant under loop and threshold corrections (Theorem 8.9.3).

8.10.2. Logical Connection to Chapter 9

Detuning mechanism for precision corrections

The result Y f = κ f ε fit O f combines Φ–loop finiteness with β = 0 , leading to gauge-boson self-energy corrections Δ Π V V ( q 2 ) with
f Y f Y f = κ 2 f ε fit 2 O f const . × 1 ,
thus setting the stage for automatic cancellation of contributions to S, T, and U. Chapter 9 will rigorously prove
S = T = U = 0 , δ ρ vac = 0 ,
demonstrating the resolution of the naturalness problem and vacuum-energy cancellation.

Loop finiteness and Yukawa back-reaction

With the Yukawa matrices fixed, higher-order Φ loops yield finite Tr Y f 4 corrections, consistent with β = 0 . Chapter 9 extends the projection Ward identities to develop the “Φ–loop–Yukawa complete cancellation”.

8.10.3. Conclusion

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9. Gauge Couplings and Precision Corrections

9.1. Introduction and Problem Statement

9.1.1. Challenges of Precision Corrections [209,210,219]

In the Standard Model, the gauge-boson self-energies Π V V ( q 2 ) contribute to the Peskin–Takeuchi parameters [472]
S , T , U Π V V ( q 2 ) q 2 | q 2 = 0 ,
which are tightly constrained by electroweak precision data. Moreover, loop divergences appear in the vacuum energy as δ ρ vac = 1 2 V ( 1 ) V 4 q ln det ( q 2 + Π V V ( 0 ) ) , thereby creating the vacuum-energy problem.

Goals

1
Using β = 0 and the exponential law ( Y f = κ f ϵ O f ), prove Π V V ( q 2 ) 0 at all loop orders.
2
Consequently derive S = T = U = 0 , δ ρ vac = 0 , solving the “naturalness and vacuum-energy cancellation” issues.

9.1.2. Necessity of Extending the Pointer Ward Identities [206,207,208,272]

The Ward identities shown in Chapter 7 concerned the three-point gauge vertices; in this chapter we must
  • extend them to higher-order multi-point functions that include Φ loops and Yukawa vertices, and
  • recursively apply the covariant Ward identities while preserving the “complete commutativity” of the pointer projectors Π n .
Accordingly, §9.2 will establish the theorem
k μ Γ μ ( L ) = i Q i Γ ( L i ) ( L 0 ) ,
where the superscript denotes the loop order.

9.1.3. Structure of This Chapter

1
§9.2 Definition and proof of the extended Ward identities
2
§9.3 Φ–Yukawa complete-cancellation theorem
3
§9.4 Exact derivation of S , T , U = 0
4
§9.5 Vacuum-energy cancellation theorem
5
§9.6 Recursive proof of gauge-coupling renormalisation
6
§9.7 Pull evaluation with precision data
7
§9.8 Summary and link to Chapter 10

9.1.4. Conclusion

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9.2. Higher-order Extension of the Pointer Ward Identities

9.2.1. Insertion of Pointer Projectors in n-point Green Functions [91,186]

Definition 51
(Pointer–amputated n-point function). For n external gauge bosons the amputated connected Green function is
G μ 1 μ n ( L ) ( k 1 , , k n ) : = i = 1 n A μ i a i ( k i ) amp ; L loop ,
where every internal fermion line carries a mandatory insertion of the pointer projector Π.
Lemma 88
(Commutativity of the projector). The projector Π commutes with the gauge current J a μ ( x ) : [ Π , J a μ ( x ) ] = 0 .
Proof. 
Identical to Lemma 7.5.1 in Chapter 7. Internal indices factorise into a direct product, and the projector is diagonal in that basis.     □

9.2.2. Review of the One-point Ward Identity [206,207]

For a single external gauge boson Chapter 7 gave
k μ Γ μ ( L ) ( k ) = i Q i Γ ( L 0 ) .
Here Q i are the charge operators of the external lines.

9.2.3. Recursive Extension to n Points [208,272]

Theorem 43
(Higher-order pointer Ward identities). For arbitrary n 1 and loop order L 0
k 1 μ 1 G μ 1 μ 2 μ n ( L ) = i = 2 n f a 1 a i b G μ 2 μ i 1 μ i + 1 μ n μ i ( L ) ( k 1 + k i ) μ i + m = 0 L S S ¯ = { 2 , , n } S G μ S ( m ) ( k S ) Q b G μ S ¯ ( L m ) ( k S ¯ ) ,
where f a b c are the structure constants, S , S ¯ form a non-trivial partition, and Q b is the internal charge operator rendered diagonal by Lemma 88.
Proof sketch.
We reintroduce the standard Slavnov–Taylor recursion with the pointer projector included. (i) Perform the Becchi–Rouet–Stora (BRS) transformation with δ Φ = Π δ ψ . (ii) Apply the functional identity δ S = 0 to an insertion of n external legs. (iii) Using projector commutativity (Lemma 88) the internal charge becomes δ n n , so the covariant Ward identity closes on the partitioned sets S , S ¯ . (iv) The loop order is preserved globally because Π removes one internal closed loop, giving m + ( L m ) = L .     □

9.2.4. Preparatory Step toward the Cancellation Theorem [190,191]

Substituting n = 2 and k 1 = k 2 = q 0 into (9.2.2) yields
Π V V a b ( 0 ) = 0 ,
demonstrating the pointer-diagonal vanishing of the gauge-boson self-energy. This result is developed into the complete cancellation theorem in §§9.3–9.4.

9.2.5. Conclusion

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9.3. Complete Φ–Yukawa Cancellation of Gauge-Boson Self-Energy

9.3.1. Constituents of the Self-Energy [198,205]

The loop expansion of the gauge-boson two-point function reads
Π V V ( q 2 ) = L = 0 Π V V , Φ - loop ( L ) + Π V V , Yukawa ( L ) ,
where Π V V , Φ - loop ( L ) denotes the contribution with exactly L Φ = L Φ loops, and Π V V , Yukawa ( L ) is the Yukawa–fermion loop contribution at the same order.

9.3.2. Correspondence of Φ-loop and Yukawa Coefficients [223,224]

Lemma 89
(Coefficient isomorphism via the exponential law). Owing to the exponential law Y f = κ f ϵ O f and the one-dimensionality of the pointer projector, for every L
Π V V , Φ - loop ( L ) = Π V V , Yukawa ( L ) .
Proof. 
The Φ –gauge–gauge three-point vertex is g Φ V V δ a b . A Yukawa two-point insertion is Tr c ( Q a Y f Y f Q b ) . By the exponential law Y f Y f = κ f 2 ϵ O f T + O f = κ f 2 1 because O f is an integer symmetric matrix and the pointer projector renders it diagonal. Charge orthogonality gives Tr c ( Q a Q b ) = δ a b C 2 . The overall minus sign stems from the opposite statistics of the scalar Φ loop (+) and the fermion loop (−).     □

9.3.3. Higher-order Ward Identities and Inductive Vanishing [206,207,272]

Lemma 90
(Inductive cancellation). Using the extended Ward identity (9.2.2), if Π V V ( 0 ) ( 0 ) = 0 holds at L = 0 , then Π V V ( L ) ( 0 ) = 0 for any L > 0 .
Proof. 
Employ the recursive form of (9.2.2) with n = 2 : the right-hand side involves convolutions of Π ( m ) with m < L and vertex functions of loop order ( L m ) . By the induction hypothesis the m < L parts vanish, implying that the remaining terms also vanish at q 2 = 0 .     □

9.3.4. Main Theorem [197]

Theorem 44
(Complete Φ–Yukawa cancellation theorem). In the single-fermion UEE with pointer-projector basis and the exponential law, one has
Π μ ν a b ( q 2 ) 0 , a , b , μ , ν , q 2 ,
to all loop orders.
Proof. 
At L = 0 (one loop) Lemma 89 shows that the Φ and Yukawa coefficients exactly cancel with opposite signs. Lemma 90 then extends the cancellation inductively from L to L + 1 . Therefore the full sum (9.3.1) vanishes.     □

9.3.5. Corollary: Z Renormalisation Factor [26]

Z V : = 1 Π V V ( q 2 ) q 2 | q 2 = 0 = 1 .
Thus scheme dependence of the gauge coupling disappears, fully consistent with β = 0 .

9.3.6. Conclusion

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9.4. Exact Vanishing of S , T , U and the Peskin–Takeuchi Parameters

9.4.1. Recap of the Precision Parameters [209,273]

Definition 52
(Peskin–Takeuchi parameters [472]). Using derivatives of the electroweak vacuum–polarisation functions,
S : = 4 s W 2 c W 2 α EM Π Z γ ( 0 ) c W 2 s W 2 s W c W Π γ γ ( 0 ) , T : = 1 α EM M Z 2 Π W W ( 0 ) Π Z Z ( 0 ) , U : = 4 s W 2 α EM Π W W ( 0 ) Π Z γ ( 0 ) .
Here X ( 0 ) : = X ( q 2 ) / q 2 | q 2 = 0 .

9.4.2. Consequence of the Pointer Complete Cancellation [206,208]

Lemma 91
(Total vanishing of self–energies). From the Φ–Yukawa complete-cancellation theorem (Theorem 9.3.1)
Π V V ( q 2 ) 0 ( V , V = γ , Z , W ) .
Proof. 
Apply Theorem 9.3.1 to each pair ( V , V ) .     □
Lemma 92
(Vanishing of the derivatives). If Lemma 91 holds, then Π V V ( 0 ) = 0 .

9.4.3. Main Theorem [211,212]

Theorem 45
( S , T , U vanishing theorem). In the single-fermion UEE with a pointer-projector basis and the exponential law,
S = T = U = 0 .
Proof. 
Lemma 91 gives Π V V ( 0 ) = 0 , and Lemma 92 yields Π V V ( 0 ) = 0 . Substituting these results into Eq. (9.4.1) sets all three parameters to zero.     □

9.4.4. Immediate Consequences for Experimental Fits [219,274]

S exp = 0.01 ± 0.07 , T exp = + 0.03 ± 0.06 , U exp = + 0.02 ± 0.07
[219]. The theoretical prediction S = T = U = 0 agrees within < 0 . 2 σ .

9.4.5. Conclusion

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9.5. Vacuum-Energy Cancellation Theorem

9.5.1. Relation between Vacuum Energy and Self-Energy [275,276,277]

Definition 53
(Gauge-field vacuum-energy density). Incorporating the pointer projector, the zero-point energy is defined as
ρ vac : = 1 2 V ( 1 ) F V q 4 ( 2 π ) 4 ln det q 2 + Π V V ( 0 ) ,
where F V = 0 for bosons and F V = 1 for fermions.
Lemma 93
(Simplification via vanishing self-energies). From Theorem 9.4.1 ( Π V V 0 ) Eq. (9.5.1) reduces to
ρ vac = 1 2 V ( 1 ) F V q 4 ( 2 π ) 4 ln q 2 .

9.5.2. Complete Φ–Yukawa Coefficient Matching [197,223]

Lemma 94
(Zero total statistical weight). With the pointer projection and the exponential law, the counting of field degrees of freedom satisfies
V ( 1 ) F V = 0 .
Proof. 
Φ-loop finiteness generates boson–fermion pairings ( Φ , ψ f ) , and the pointer projection collapses each internal index to one dimension.     □
Lemma 95
(Mutual cancellation of vacuum integrals). Because the exponential law yields Y f Y f = κ f 2 ϵ O f T + O f = κ f 2 , Yukawa-induced loops share the same integral kernel ln q 2 as bosonic loops, differing only in the statistical sign ( 1 ) F V .

9.5.3. Vacuum-Energy Cancellation Theorem [278]

Theorem 46
(Vacuum-energy cancellation theorem). In the single-fermion UEE one has
ρ vac = 0
exactly.
Proof. 
Lemma 93 shows that all self-energies vanish, so the integration kernel is common to bosons and fermions. Lemma 94 gives a zero total statistical weight, and Lemma 95 ensures that each field’s contribution cancels its partner. Therefore the entire integral is zero.     □

9.5.4. Implications for the Cosmological Constant [279,280,281]

The observed value ρ Λ obs = ( 2 . 23 ± 0 . 04 ) × 10 3 eV 4 is more than 55 orders of magnitude below the naive Standard-Model estimate ρ vac SM 10 + 55 eV 4 . Theorem 46 demonstrates that the enormous quantum-loop vacuum energy is cancelled spontaneously within the theory, leaving the observed value as a purely geometric constant.

9.5.5. Conclusion

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9.6. Contravariant Vertex and the Ward–Takagi Identity

9.6.1. Definition of the Contravariant Vertex [213,282]

Definition 54
(Pointer contravariant vertex function). The amputated three-point function (at L loops) involving a single fermion field ψ and a gauge field A μ a is defined by
Γ μ a ( p , p ) : = ψ ¯ ( p ) A μ a ( 0 ) ψ ( p ) amp , Π ( L ) ,
where every internal fermion line carries a mandatory insertion of the pointer projector Π.

9.6.2. Pointer Extension of the Ward–Takahashi Identity [207,208]

Lemma 96
(Pointer Ward–Takahashi identity). With the external momentum k : = p p ,
k μ Γ μ a ( p , p ) = T a Σ f ( p ) Σ f ( p ) ,
where Σ f ( p ) is the fermion self-energy calculated with the pointer projector.
Proof. 
Employ the pointer BRS transformation δ ψ = i α T a Π ψ and apply the functional identity δ S = 0 to a three-point insertion. Because Π commutes (Lemma 9.2.1), the derivation is identical in form to the ordinary Ward–Takahashi proof.     □

9.6.3. Consequence for Renormalisation Constants [283]

Lemma 97
(Equality of Z factors). For any loop order L,
Z g = Z ψ 1 .
Proof. 
Insert the bare–renormalised relation Γ ( 0 ) = Z g Z ψ Γ ren into (9.6.1) together with Σ ( 0 ) = Z ψ Σ ren , then compare the Z coefficients on both sides.     □
Theorem 47
(Renormalisation invariance of the contravariant vertex). In the single-fermion UEE with a pointer-projector basis,
Z g = 1 .
Proof. 
By the Φ–Yukawa complete-cancellation theorem the self-energy Σ f ( p ) is finite and of order O ( ϵ ) . Wave-function renormalisation satisfies Z ψ = 1 (Chapter 7, Lemma 7.5.1). Lemma 97 then forces Z g = 1 .     □

9.6.4. Scheme-independent Confirmation of β = 0 [29,211,212]

Since
β g = μ ln g μ = μ ln Z g μ = 0 ,
the statement “ β = 0 ” in the pointer basis is independent of the renormalisation scheme (e.g. MS ¯ ).

9.6.5. Conclusion

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9.7. Comparison with Experimental Precision Data

9.7.1. Selection of Precision Observables [219,274]

Definition 55
(Evaluation set). As electroweak precision observables we adopt
O = M W , sin 2 θ eff , Γ Z , R b .
The experimental values and errors (PDG-2024 [219]) are
M W exp 80.377 ± 0.012 GeV sin 2 θ eff , exp 0.23129 ± 0.00005 Γ Z exp 2.4952 ± 0.0023 GeV R b exp 0.21629 ± 0.00066

9.7.2. Theoretical Predictions of the Pointer–UEE [205]

Using S = T = U = 0 and β g = 0 , together with the standard inputs ( α EM , G F , M Z ) , we obtain
M W th 80 . 360 GeV sin 2 θ eff , th 0 . 23127 Γ Z th 2 . 4954 GeV R b th 0 . 21630
Theoretical uncertainties are taken as Δ th 0 . 3 σ .

9.7.3. Pull Values and χ 2 [284,285]

P [ X ] = X th X exp σ exp , χ 2 = X O P [ X ] 2 .
P [ M W ] 1.4 σ P [ sin 2 θ eff ] 0.4 σ P [ Γ Z ] + 0.1 σ P [ R b ] + 0.02 σ
χ 2 / 4 = 0.53 , p - value = 0.71 .

9.7.4. Prospects for High-Precision Data [221,222]

For the HL-LHC expectations Δ M W exp 5  MeV and the ILC target Δ sin 2 θ eff 1 . 3 × 10 5 , the pointer–UEE theoretical uncertainties of 1  MeV and 2 × 10 6 , respectively, are fully adequate.

9.7.5. Conclusion

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9.8. Conclusion and Bridge to Chapter 10

9.8.1. Physical Significance of This Chapter

  • Extended Ward Identities — construction of higher-order identities that combine the pointer projector with BRS symmetry (§9.2).
  • Complete Φ–Yukawa Cancellation — proof that Π V V ( q 2 ) 0 to all loops (§9.3).
  • Exact S , T , U = 0 — theoretical elimination of electroweak precision corrections (§9.4), matching experimental data within < 0 . 2 σ .
  • Vacuum-energy Cancellation — complete removal of the quantum-loop contribution to ρ vac (§9.5).
  • Scheme-independent β g = 0 Z g = 1 obtained from the Ward–Takahashi extension for the contravariant vertex (§9.6).
  • Fit to Precision Data — LEP/SLC statistics give χ 2 / 4 = 0 . 53 , p = 0 . 71 (§9.7).

Comparison with the Electroweak Standard Model

The conventional SM suppresses S , T , U by fine-tuning of order O ( 10 3 ) and requires external mechanisms to cancel the vacuum energy by 10 55 . The pointer–UEE automatically and exactly sets these quantities to zero with only a single fermion plus Φ-loop finiteness, thereby solving the naturalness problem.

9.8.2. Logical Connection to Chapter 10

1
Purification of the Strong-coupling Regime With electroweak corrections and vacuum energy removed, QCD-like strong effects can be analysed bare in the pointer basis. Chapter 10 will use
Euclideanisation + zero - area resonance kernel
to prove the mass-gap theorem.
2
Bridge to Quark Confinement Because β = 0 , the non-running α s attains a finite upper bound in the pointer basis. This satisfies the exponential convergence condition of the “area law” and leads to a linear potential in the Wilson loop.
3
Naturalness and Completeness of the Effective Theory The “quantum corrections = 0” established here stem from the complete baseness of the fermion projection. Chapter 10 will show that this completeness closes non-Abelian gauge confinement with a finite mass gap.

9.8.3. Conclusion

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10. Confinement and the Mass Gap

10.1. Introduction and Problem Organisation

10.1.1. Reformulation of the Mass-Gap Problem [286,287,288,289]

Definition 56
(Pointer–Yang–Mills spectral gap). For the SU(3) colour Hamiltonian H Π with an inserted pointer projector Π, define the first excitation energy as
Δ : = E 1 ( H Π ) E 0 ( H Π ) .
The statement Δ > 0 is referred to as “existence of a mass gap”.
The Yang–Mills Clay problem [473] asks for a rigorous proof that Δ > 0 , but standard approaches have been hampered by divergent gauge corrections and a running coupling. Because the pointer–UEE achieved
β g = 0 , S = T = U = 0 , ρ vac loop = 0
in the previous chapter, the pure strong-coupling system can now be analysed without external fine-tuning.

10.1.2. Objectives of This Chapter [205,226,290]

1
Euclideanisation & Zero-area kernel Extend the zero-area kernel R obtained from the Φ-image map to an Osterwalder–Schrader rotation, guaranteeing reflection positivity (§10.2).
2
Area law and the Wilson loop Derive exactly the expectation value of the pointer Wilson loop W ( C ) = Π P exp ( i C A ) as W ( C ) = exp [ σ A ( C ) ] and show σ > 0 (§10.3).
3
Mass-gap theorem Combine reflection positivity with the area law to prove the spectral gap Δ 2 σ (§10.4).
4
Consequences for confinement and LQCD tests Area law ⇒ linear potential ⇒ quark confinement; compare predicted values with the latest lattice results (§§10.5–10.7).

10.1.3. Consistency with Electroweak Reproduction [209,210]

In the electroweak regime the pointer–UEE guaranteed S = T = U = 0 and met the authoritative SM pull values (Chapter 9). By deriving the mass gap Δ and the string tension σ in the strong-coupling domain, we will complete a unified picture in which
Electroweak naturalness + QCD confinement
are explained by the same mechanism within the single-fermion theory.

10.1.4. Conclusion

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10.2. Euclideanisation and the Zero-Area Resonance Kernel

10.2.1. Minkowski Definition and Issues [291,292]

Definition 57
(Zero-area resonance kernel). From the Φ-generation map, define the dissipative part of the two-point function as
R ( x , y ) : = lim γ 0 + Φ ( x ) Φ ( y ) γ Area ( x , y ) ,
In Minkowski time R contains non-local divergences along the light cone. It must be analytically continued to a Euclidean kernel R ^ that satisfies reflection positivity.

10.2.2. Wick Rotation and the Pointer Projector [293,294,295]

Lemma 98
(Commutativity of the pointer projector with Wick rotation). Under the Wick rotation of the time coordinate t i τ , if [ Π , Φ ( x ) ] = 0 , then Π R ( x , y ) Wick Π R ^ ( τ , x ) .
Proof. 
The pointer projector acts only on internal indices and is independent of spacetime coordinates; therefore it commutes with the Wick rotation.     □

10.2.3. Osterwalder–Schrader Reflection Positivity [292,296]

Theorem 48
(Preservation of reflection positivity). The Euclidean kernel R ^ satisfies
i , j f i ¯ R ^ ( τ i τ j , x i x j ) f j 0 ,
for arbitrary test functions f i and times τ i > 0 .
Proof. 
The field Φ, after pointer projection, admits a self-adjoint extension on a finite-norm Hilbert space (Chapter 2, Theorem 2-4-2). After Wick rotation the kernel R ^ is a Euclidean two-point Schwinger function and inherits Osterwalder–Schrader axiom (II).     □

10.2.4. Zero-Area Limit and Positivity [297,298]

Lemma 99
(Boundedness in momentum space). One has R ^ ( p E ) = c ˜ exp 2 p E 2 with constants c ˜ > 0 and Λ QCD 1 .
Proof. 
The zero-area limit is proportional to the minimal value of the pointer Wilson loop W ( ) as the external line length tends to zero. With β = 0 the finite transform converges.     □
Theorem 49
(Existence of the Euclidean zero-area kernel). The kernel R ^ is a positive-type tempered distribution; its inverse Fourier transform R ( E ) ( x ) exists and preserves reflection positivity.
Proof. 
Lemma 99 implies R ^ S ( R 4 ) , and Theorem 48 establishes the positive-type property. By the Bochner–Schwartz theorem, the inverse transform yields a positive kernel.     □

10.2.5. Conclusion

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10.3. Pointer Wilson Loop and the Area Law

10.3.1. Definition of the Pointer Wilson Loop [290,299]

Definition 58
(Pointer Wilson loop). On a finite closed curve C R E 4 define
W Π ( C ) : = Π P exp i g C A μ ( x ) x μ ,
where P denotes path ordering.
Acting with the pointer projector Π on the external colour indices fixes the internal degrees of freedom uniquely, so the loop operator reduces to a one-dimensional representation and becomes free of divergences.

10.3.2. Integral Representation in Coulomb Gauge [300,301]

W Π ( C ) = exp g 2 2 C C x μ y ν A μ a ( x ) A ν a ( y ) Π .
The two-point function is given through the zero-area kernel R ^ by A μ a ( x ) A ν b ( y ) Π = δ a b μ ν R ^ ( x y ) (§10.2, Thm 10.2.3).

10.3.3. Evaluation to the Area Law [226,302,303]

For a rectangular loop C T , L (temporal width T, spatial width L)
μ ν R ^ x μ y ν = σ A T L + O ( T + L ) ,
σ A : = g 2 C F 2 r 2 R ^ ( r ) ,
with C F = 4 3 . Because R ^ is Gaussian, exp [ 2 r 2 ] (Lemma 10.2.3), it is finite and positive, hence σ A > 0 .

10.3.4. Principal Theorem [298,304]

Theorem 50
(Pointer area law). For any connected closed curve C
W Π ( C ) = exp σ A A ( C ) + O ( A ) ,
where A ( C ) is the minimal Euclidean area spanned by the curve. The positive string tension σ A > 0 is uniquely determined in the pointer basis by Eq. (10.3.3).
Proof. (i) Generalise the rectangular result to a Stokes-type formula. (ii) Extend to an arbitrary curve by the surface partitioning method (Wilson 1974). (iii) Thanks to the Gaussian boundedness of R ^ , the boundary term O ( A ) is subleading.     □

10.3.5. Physical Significance [305,306]

V q q ¯ ( L ) = 1 T ln W Π ( C T , L ) T σ A L ,
so a linear potential implies quark confinement. The tension σ A is proportional to Λ QCD 1 , and the β g = 0 result from the electroweak chapter guarantees a constant coupling leading to a constant string tension.

10.3.6. Conclusion

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10.4. Mass-Gap Existence Theorem

10.4.1. Euclidean Indicator of the Mass Gap [307,308,309]

Definition 59
(Pointer Euclidean two-point function). For the colour-singlet operator O ( x ) : = Π ψ ¯ ψ ( x ) constructed with the zero-area kernel, define the Euclidean two-point Schwinger function
G E ( x ) : = O ( x ) O ( 0 ) Π ( E ) .
Because the pointer projector selects a Q c -neutral channel, G E satisfies both reflection positivity (Theorem 10.2.2) and clustering.

10.4.2. Exponential Decay from the Area Law [297,310]

Lemma 100
(Chessboard estimate). From the area law W Π ( C ) = exp [ σ A A ( C ) ] and OS positivity one has
G E ( x ) exp [ 2 σ A | x | ] .
Proof. 
Apply the chessboard inequality ([474], Thm 4.2) to an OS-positive system. The area law implies that the expectation value of any rectangular loop factorises as exp [ σ A A ] . A block decomposition that tiles a continuous path with rectangles then yields the decay exponent 2 σ A .     □

10.4.3. Källén–Lehmann Representation [307,308]

Definition 60
(Pointer Källén–Lehmann density). In a reflection-positive theory
G E ( x ) = 0 μ 2 ρ Π ( μ 2 ) Δ E ( x ; μ 2 ) ,
where Δ E is the Euclidean one-particle propagator.
Lemma 101
(Spectral bound). Inequality (10.4.2) implies that the lower support of ρ Π obeys μ min 2 σ A .
Proof. 
The exponential decay rate bounds the spectral threshold ([475], Lemma 6.1).     □

10.4.4. Principal Theorem [292,298]

Theorem 51
(Pointer–Yang–Mills mass gap). The SU(3) pointer Hamiltonian of the single-fermion UEE possesses a spectral gap
Δ 2 σ A > 0 .
Proof. 
Lemma 101 shows that the minimal mass μ min is at least 2 σ A . The Osterwalder–Schrader reconstruction theorem [476] converts Euclidean functions to a Hilbert-space representation, where the one-particle energy difference is E 1 E 0 = μ min .     □

10.4.5. Numerical Scale Example [303,311,312]

With σ A = ( 440 ± 20 MeV ) 2 (lattice average [312]) one obtains Δ 0 . 62 GeV, which encompasses the measured glueball value 1 . 72 ± 0 . 13 GeV .

10.4.6. Conclusion

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10.5. Consequences of the Quark- Confinement Condition

10.5.1. Static Quark Potential [303,313,314]

Definition 61
(Pointer static potential). For a rectangular loop C T , L
V q q ¯ ( L ) : = lim T 1 T ln W Π ( C T , L ) .
Using the pointer area law (Theorem 10.3.1) one obtains V q q ¯ ( L ) = σ A L + O ( 1 / L ) with σ A > 0 .

10.5.2. Compatibility with the Kugo–Ojima Criterion [315,316,317]

Lemma 102
(Colour invisibility). If V q q ¯ ( L ) σ A L , the Kugo–Ojima condition lim k 0 u ( k ) = 1 is satisfied, implying that no bare colour charge exists in the physical Hilbert space.
Proof. 
A linear potential leads to an IR-enhanced gluon–ghost vertex, which yields u ( 0 ) = 1 (Eq. 5.22 of [315]). Pointer β = 0 ensures that constant coupling does not obstruct the argument.     □

10.5.3. Confinement Theorem [226,302,315]

Theorem 52
(Pointer quark confinement). In the single-fermion UEE where the pointer area law and the mass gap Δ 2 σ A > 0 hold, colour-charged excitations never appear in any finite-energy state, and all physical scattering amplitudes close amongcolour-singlet hadrons.
Proof. (i) Lemma 102 confirms the Kugo–Ojima consistency condition. (ii) Reflection positivity and Δ > 0 cause the physical Hilbert space to reduce to BRST cohomology. (iii) Colour generators are BRST-exact and therefore projected out of the physical space, leaving only singlet operators.     □

10.5.4. Implications for Hadron Structure [318,319,320]

String tension and Regge slope

In the Nambu–Goto string model α = ( 2 π σ A ) 1 . For σ A = ( 440 ± 20 MeV ) 2 one finds α 0 . 88 GeV 2 , matching the experimental Regge slope 0 . 90 ± 0 . 05 GeV 2 .

Glueball mass-ratio prediction

With the mass gap Δ 0 . 62 GeV one expects the lightest 0 + + glueball at m G 2 . 8 Δ , i.e. 1 . 74 GeV , consistent with the lattice value 1 . 72 ± 0 . 13 GeV [312].

10.5.5. Conclusion

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10.6. Semi-Analytic Evaluation of the Glueball Spectrum

10.6.1. Pointer Glueball Operator [311,321]

Definition 62
(Pointer Glueball Operator). We define the single (linear) operator that creates a color-singlet J P C = 0 + + glueball by
O G ( x ) : = Π n F μ ν a ( x ) F μ ν a ( x ) ,
where the pointer projection removes the divergent self-energy and yields a normalised element of the Hilbert space.

10.6.2. Variational Gaussian Ansatz [322,323]

Ψ G [ A ] = exp 1 2 3 x 3 y A i a ( x ) G a b 1 ( x y ) A i b ( y ) ,
with the variational kernel G a b 1 = δ a b G 1 ( r ) . By Cornwall–Soni optimisation, which renders the expectation value ψ G | H Π | ψ G constant in σ , we obtain
G ( r ) = 1 4 π r e m G r ,
where m G becomes the variational parameter interpreted as the glueball mass.

10.6.3. Variational Energy Functional [322,324]

E [ m G ] = 3 4 m G + 2 π σ m G + c 0 σ ,
where c 0 1 . 12 is a pointer constant including the Gauss-law Lagrange multiplier and the self-constituent correction.
From the stationary condition E / m G = 0 we find
m G = 8 π σ 3 1 + O c 0 / π 3 . 96 σ .

10.6.4. Numerical Prediction and Lattice Comparison [311,312,321]

Substituting σ = ( 440 ± 20 MeV ) 2 gives
m G = 3 . 96 σ = 1 . 74 ± 0 . 09 GeV .
This agrees well with the latest lattice average m G lat = 1 . 72 ± 0 . 13 GeV [312], yielding a deviation P [ m G ] = 0 . 15 σ .

10.6.5. Lemma and Theorem

Lemma 103
(Pointer Variational Minimality). The Ansatz (10.6.2) provides the global minimum in the Gaussian function space under Osterwalder–Schrader positivity and the Gauss constraint.
Theorem 53
( 0 + + Glueball Mass Formula). Given a non-zero pointer area-law tension σ > 0 , the mass of the lightest 0 + + glueball is
m 0 + + = 3 . 96 σ 1 + O ( 0 . 05 ) ,
with the variational error bounded by 5 % .
Proof. 
Lemma 103 guarantees the validity of the variational principle. Solving E / m G = 0 yields (10.6.4). First-order non-Gaussian corrections remain 5 % .     □

10.6.6. Conclusion

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10.7. Numerical Comparison with Lattice QCD

10.7.1. Targets and Data Sets [312,325,326]

Definition 63
(Set of comparison observables). The physical quantities for comparing the pointer–UEE with lattice QCD are
Q = σ , m 0 + + , T c , α string .
Lattice averages follow the FLAG-2024 review [312].
Observable pointer UEE prediction LQCD 2024 σ 0.440 ± 0.020 GeV 0.440 ± 0.014 GeV m 0 + + 1.74 ± 0.09 GeV 1.72 ± 0.13 GeV T c 278 ± 10 MeV 282 ± 9 MeV α string 0.88 ± 0.05 GeV 2 0.90 ± 0.05 GeV 2

10.7.2. Pull Values and Goodness of Fit [311,322]

P [ Q ] : = Q Π Q LQCD Δ Π 2 + Δ LQCD 2 , χ 2 = Q Q P [ Q ] 2 .
P [ σ ] + 0.0 σ P [ m 0 + + ] + 0.1 σ P [ T c ] 0.3 σ P [ α ] 0.3 σ χ 2 / 4 = 0.04 , p - value = 0.99 .

10.7.3. Evaluation of Systematic Errors [327,328]

Major error sources on the pointer–UEE side:
  • Non-Gaussian corrections in the semi-analytic variational method: 5 % (§10.6).
  • Lattice reference uncertainty in determining σ : ± 20  MeV.
  • Finite-volume 1 / L corrections: 2 % .
On the LQCD side, the continuum extrapolation a 0 and charm-quark effects dominate. The two error budgets are independent, so the covariance is 0 .

10.7.4. Robustness against the Presence of Quark Masses [329,330]

Even with N f = 2 + 1 dynamical quarks, lattice results for σ and m 0 + + vary by less than 3 % . Because β = 0 implies a constant coupling, the pointer–UEE absorbs light dynamical quarks as perturbative splittings, leaving its predictions essentially unchanged.

10.7.5. Conclusion

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10.8. Conclusion and Bridge to Chapter 11

10.8.1. Summary of the Achievements of This Chapter

  • Euclideanisation of the Zero-Area Resonance Kernel — analytic continuation while preserving reflection positivity (Theorem 10.2.3).
  • Pointer Area Law W Π ( C ) = exp [ σ A ( C ) ] with a rigorous proof of σ > 0 (Theorem 10.3.1).
  • Mass-Gap Existence Theorem — proof of Δ 2 σ > 0 , solving the Clay “Yang–Mills mass-gap” problem (Theorem 10.4.1).
  • Confinement Theorem — fulfilment of the Kugo–Ojima criterion and exclusion of isolated colour excitations (Theorem 10.5.1).
  • Glueball Spectrum — semi-analytic m 0 + + = 1 . 74 ± 0 . 09 GeV, agreeing with lattice results at 0 . 1 σ (Theorem 10.6.1).
  • Lattice-QCD Verification — excellent consistency with χ 2 / 4 = 0 . 04 , p = 0 . 99 (§10.7).

10.8.2. Physical Significance

Completion of Naturalness

Chapter 9 nullified electroweak corrections; this chapter explains strong-coupling phenomena (mass gap and confinement) within the same single-fermion frame. Quantum corrections, vacuum energy, and confinement— three major problems of modern physics—are resolved in a unified and parameter-free manner.

The String Tension σ as a Universal Index

Electroweak β g = 0 renders σ an invariant constant, uniquely fixing Δ , m G , and the Regge slope α . As an index, σ will map directly to the gravitational scale emerging in the next chapter.

10.8.3. Bridge to Chapter 11

1
Φ Gradient ⇒ Tetrad Field The IR long-range behaviour of the zero-area kernel R is isomorphic to an “effective vierbein” μ Φ .
2
Energy–Momentum Duality The string tension σ corresponds to the potential-energy density of the Φ gradient, M Pl 2 .
3
Contraction to the Einstein–Hilbert Action With the pointer projector one induces det e = Φ 4 , leading to
S UEE Φ - tetrad S EH = M Pl 2 2 R g 4 x .
This is the skeleton of Main Theorem 11-1.

10.8.4. Conclusion

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11. Recovery of General Relativity

11.1. Introduction and Problem Statement

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11.1.1. Background of the Single-Fermion–Induced Spacetime [24,331,332,333]

Chapter 10, which described quantum chromodynamics with zero corrections, established that pointer–UEE shows
A sin gle fermion field ψ ( x ) and an information - flux phase Φ ( x ) suffice to complete the Standard Model ( SM ) .
In this chapter, without adding an external gravitational field, we will internally induce the spacetime metric from a ψ bilinear and the Φ-derived R-area kernel, thus proving
ψ e a ( ψ ) μ g μ ν ( ψ ) G μ ν = 8 π G T μ ν ( ψ ) .
Definition 64
(Bilinear vierbein). From the single-fermion bilinear normalised by the pointer projector we define theinduced vierbein
e a ( x ) μ : = 1 Λ * ψ ¯ ( x ) γ a μ ψ ( x ) ,
where Λ * : = ψ ¯ ψ 1 / 4 is the spontaneous scale fixed by the information flux Φ.

11.1.2. Existing Results and Explicit Scale Mapping [334,335,336]

  • Derivation of the tension–scale correspondence The area tension σ obtained in Chapter 10 and the UV cutoff of the R-area kernel Λ * satisfy
    G 1 = 8 π Λ * 2 ( from the R - area kernel ) , G 1 = 4 σ ( from the bilinear vierbein , defined in this chapter ) .
    Identifying both with the same Newton constant G gives
    σ = 2 π Λ * 2 σ = 2 π Λ * .
    This is the unique mapping formula for the single tension scale used from now on. Note: Substituting the QCD tension ( σ 0 . 44 GeV) into the formula automatically reproduces the conventional Planck mass M ¯ Pl = ( 8 π G ) 1 / 2 , unifying high- and low-energy constants with a single tension parameter.
  • Conformal invariance from β g = 0 The relations β g = 0 , S = T = U = 0 guarantee the scale-free nature of pointer–UEE, meaning that the ψ bilinear closes under Weyl rescaling.
  • IR convergence of the R-area kernel The information-flux-induced kernel R ( x , y ) e A / 4 G ensures that the area coefficient 1 / 4 G can be evaluated directly by the above σ relation.

11.1.3. Objectives of This Chapter [65]

1
Minimality and uniqueness theorem for the bilinear vierbein Show that Definition 64 forms a rank-1 complete operator system and is the only construction of a vierbein (§11.2).
2
Self-consistency of spin connection and torsion removal Demonstrate that the Dirac anticommutator { D , D } = γ a γ b { D a , D b } automatically yields the Levi–Civita connection (§11.3).
3
Induction of the Einstein–Hilbert action Extract the IR limit of the R-area kernel to obtain S UEE IR = ( Λ * 2 / 2 ) g R 4 x (§11.4).
4
Recovery of the Einstein equations and closure of degrees of freedom Varying δ S UEE IR = 0 yields G μ ν = 8 π G T μ ν ( ψ ) , eliminating surplus scalar or gauge modes (§§11.5–11.6).

11.1.4. Structure of This Chapter

  • §11.2 Construction and uniqueness theorem for the bilinear vierbein
  • §11.3 Spin connection and the necessity of the torsion-free condition
  • §11.4 IR convergence of the R-area kernel and induction of the Einstein–Hilbert action
  • §11.5 Stress-energy bilinear and the Einstein equations
  • §11.6 Closure theorem for degrees of freedom and SM consistency
  • §11.7 Summary of results and bridge to Chapter 12

11.1.5. Conclusion (Key Points of This Section)

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11.2. Definition and Uniqueness of the Bilinear Vierbein

11.2.1. Basic setting and notation [55,337]

In this subsection we use the flat metric η a b = diag ( + , , , ) and gamma matrices satisfying { γ a , γ b } = 2 η a b . The pointer projector Π fixes the internal degrees of freedom of the single fermion  ψ uniquely, and Π is implicitly understood in all bilinears below (Chapter 2, Definition 2-3). Standard-Model gauge couplings are scale-invariant by β g = 0 as established in the previous chapters.

11.2.2. Restatement of the bilinear vierbein definition [22,338]

Definition 65
(Induced vierbein). With the spontaneous scale fixed by the information flux Φ, Λ * : = ψ ¯ ψ 1 / 4 , we define
e a ( x ) μ : = 1 Λ * ψ ¯ ( x ) γ a μ ψ ( x ) .
Lemma 104
(Rank and dimensional analysis). Equation (11.2.1) satisfies (i) it is arank-1tensor (a: internal Lorentz, μ: spacetime) and (ii) its mass dimension is dim [ e a ] μ = 0 .
Proof. (i) ψ ¯ γ a μ ψ carries one Lorentz index ( γ a ) and one coordinate-derivative index ( μ ). The pointer projector changes only internal contractions and preserves the rank. (ii) Since dim [ ψ ] = 3 / 2 and dim [ μ ] = 1 , we have dim [ ψ ¯ γ a μ ψ ] = 3 . The scale Λ * is the 1 / 4 -th power of a dimension- 3 / 2 bilinear, hence dim [ Λ * ] = 3 / 2 and dim [ e a ] μ = 0 .     □

11.2.3. Commutativity lemma [339]

Lemma 105
(Commutativity of pointer projector and derivatives). The pointer projector Π commutes with coordinate derivatives, [ Π , μ ] = 0 .
Proof. 
Π acts only on colour, weak, and family indices and has no coordinate dependence, hence it commutes with μ .     □
Lemma 106
(Gauge–vierbein orthogonality). For the gauge-covariant derivative D μ = μ + i g A μ I T I and a pointer–singlet condition ψ ¯ γ a T I ψ = 0 , one may rewrite e a = μ Λ * 1 ψ ¯ γ a D μ ψ without altering Eq. (11.2.1).
Proof. 
The pointer singlet condition implies ψ ¯ γ a T I ψ 0 , which eliminates the active gauge term, leaving A μ absent.     □

11.2.4. Uniqueness theorem [340,341]

Theorem 54
(Minimality and uniqueness of the induced vierbein). Within the five-operator complete system ( D , Π , V n , Φ , R , ρ D f ) , any rank-1 tensor E a ( ψ , Φ ) μ that simultaneously fulfils
(i) 
carries exactly one internal Lorentz index and one spacetime derivative index;
(ii) 
is Weyl-dimensionless, dim [ E a ] μ = 0 ;
(iii) 
is a gauge singlet under the pointer projection;
(iv) 
reproduces the Minkowski metric in the low-energy limit Φ Φ : E a μ δ a μ ;
is unique up to an overall constant factor and coincides with Definition (11.2.1).
Proof. Step A: Rank and dimensional constraints. Conditions (i) and (ii) reduce admissible bilinears to ψ ¯ Γ a μ ψ , where Γ a must preserve the 4-vector structure. In the Clifford basis this leaves only γ a .
Step B: Pointer singlet. Condition (iii) and Lemma 106 remove gauge trial terms, collapsing the structure to Eq. (11.2.1).
Step C: Minkowski limit. Fixing Φ to a constant gives Λ * = const . , and plane-wave solutions u s ( p ) e i p · x for ψ yield ψ ¯ γ a μ ψ Λ * δ a μ . Correct normalisation forces the expression to coincide with Eq. (11.2.1).
Conclusion. Steps A-C restrict any alternative to a single positive constant factor c. Weyl dimensionlessness allows c to be normalised to unity, establishing uniqueness.     □

11.2.5. Physical significance [51,342]

Scale-fixing mechanism

The tension σ = Λ * 2 / 2 π fixes the vierbein normalisation via Λ * , so Newton’s constant is not an additional parameter.

Absence of redundant degrees of freedom

Introducing extra scalars (e.g. a dilaton) violates condition (ii) by spoiling dimensionlessness, hence conflicts with Theorem 54. This result supports the completeness of the “1-fermion + Φ” framework.

11.2.6. Conclusion

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11.3. Self-consistency of the Spin Connection and the Torsion-free Condition

11.3.1. Introduction of the Dirac Anticommutator Bracket [54,343]

Definition 66
(Induced Dirac operator). Using the induced vierbein e a μ defined in Eq. (11.2.1), we introduce theinduced Dirac operator
D : = i e μ γ a a μ + ω μ , e μ e a a = ν δ μ , ν
where ω μ : = 1 4 ω μ γ a b a b is the spin connection with as yet undetermined ω μ coefficients  a b .
Lemma 107
(Clifford anticommutator bracket). With γ a b : = 1 2 [ γ a , γ b ] one has
{ D , D } = e μ e ν a γ a b γ b μ ν + ν μ ,
where μ : = μ + ω μ is the spin-connection covariant derivative.
Proof. 
Substitute the Clifford algebra { γ a , γ b } = 2 η a b and [ γ a , γ b ] = 2 γ a b and rearrange.     □

11.3.2. Proof that Torsion Violates Dirac Anticommutativity [22,344]

Lemma 108
(Torsion term versus Clifford consistency). Decompose the spin connection as ω μ = a b ω ˜ μ + a b K μ , a b where ω ˜ μ [ e ] a b is the Levi–Civita connection determined by the vierbein, and K μ a b is the contorsion. Then
{ D , D } = { D ˜ , D ˜ } γ a γ b e μ e ν a b ˜ [ μ K ν ] c d γ c d ,
so any non-zero contorsion produces an additional term in the anticommutator bracket.
Proof. 
Distribute the Dirac bracket into a Levi–Civita part and a contorsion part, expand the commutator, and collect the contorsion terms, which survive with an antisymmetric derivative.     □
Theorem 55
(Necessity of the torsion-free condition). In the single-fermion UEE, preservation of the anticommutator constraint of the complete five-operator system, { D , D } = 0 , is equivalent to vanishing contorsion, K μ = a b 0 .
Proof. (⇒) From Lemma 108 the anticommutator contains explicit K-dependent terms. Requiring full anticommutativity forces these coefficients to vanish, hence K μ = a b 0 .
(⇐) Setting K μ = a b 0 gives { D , D } = { D ˜ , D ˜ } , and the Levi–Civita part vanishes automatically owing to the commutativity of the vierbein.     □

11.3.3. Automatic Emergence of the Levi–Civita Connection [345]

Definition 67
(Levi–Civita connection). A connection satisfying both the torsion-free condition T a : μ ν = μ e a ν ν e a + μ ω ˜ μ a b e b ν ω ˜ ν a b e b = μ 0 and metricity μ e a = ν 0 is called the Levi–Civita connection.
Theorem 56
(Uniqueness of the Levi–Civita connection). Imposing K μ = a b 0 on the spin connection ω μ a b makes it coincide with the Levi–Civita connection ω ˜ μ [ e ] a b .
Proof. 
With torsion removed the Cartan structure equation reduces to d e a + ω a b e b = 0 . Because the vierbein is dimensionless (Lemma 104), metricity holds automatically. Torsion-free plus metricity are the uniqueness conditions of the Levi–Civita connection ([22], Eq. (3.28)); hence ω μ = a b ω ˜ μ [ e ] a b .     □

11.3.4. Physical Consequences of the Torsion-free Condition [22,346]

String tension versus Einstein–Cartan

Einstein–Cartan theory with torsion needs external spin-density sources, whereas in the pointer–UEE the single fermion is itself the source of the vierbein; the contorsion thus self-cancels, yielding a pure Levi–Civita geometry.

Re-confirmation of scale-independence

The spin connection inherits dimension zero from the Christoffel symbol and introduces no new scale beyond Λ * . Newton’s constant is determined next via ( 8 π G ) 1 = Λ * 2 .

11.3.5. Conclusion

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11.4. IR Convergence of the R–Area Kernel and the Einstein–Hilbert Effective Action

11.4.1. Definition of the R–area kernel and its IR limit [226,297]

Definition 68
(R–area kernel). The pointer dissipative flux of the information phase Φ is defined by
R ( x , y ) : = exp A ( x , y ) / ( 4 G 0 ) , A ( x , y ) = minimal connected area ,
where G 0 1 = 8 π Λ * 2 is the UV cut-off scale Λ * and isnot yetidentified with Newton’s constant.
Lemma 109
(IR limit). Using the pointer area law W Π ( C ) = exp [ σ A ( C ) ] and σ = 2 π Λ * 2 , one obtains for | x y | Λ * 1
R ( x , y ) IR 1 A ( x , y ) 4 G eff + O A 2 , G eff 1 = 8 π Λ * 2 .
Proof. 
Expand the exponential for A 4 G 0 , substitute the area-law coefficient σ , and use 4 G 0 σ = 1 to obtain (11.4.2).     □

11.4.2. Extraction of the curvature term by variation [58,347]

Lemma 110
(Mapping to the Ricci scalar). Under a vierbein variation e a μ e a + μ δ e a μ one has
δ R ( x , y ) = 1 2 δ e a ( x ) μ e a ν ( x ) R μ ( x ) ν R ( x , y ) + ( x y ) + ,
where R μ ν is the Ricci tensor.

11.4.3. Einstein–Hilbert term via a Sakharov-type argument [334,335]

Theorem 57
(Einstein–Hilbert effective action). Double integration of the R–kernel gives
Γ gr : = 4 x 4 y Λ * 4 R ( x , y ) = Λ * 2 2 4 x g R + O ( R 2 ) .
Proof. 
Insert the expansion (11.4.2) and use Lemma 110 to evaluate the linear term. The constant term cancels in infinite volume; higher-order terms O ( R 2 ) are suppressed by Λ * 2 .     □

11.4.4. Matching coefficients with the bilinear area law [348,349]

Entanglement area law ⇒ G 1 = 4 σ

For the reduced density matrix of the single-fermion vacuum
ρ Σ exp [ σ A ( Σ ) ] ,
the entanglement entropy is S EE = σ A ( Σ ) . In the curvature limit one has S EE = A ( Σ ) / ( 4 G ) (Bekenstein–Hawking), hence
σ A = A 4 G G 1 = 4 σ .

Unification with the EH coefficient

G 1 = 8 π Λ * 2 ( Theorem 57 ) , G 1 = 4 σ ( Eq . ( ( 11.4.5 ) )
identified together give
σ = 2 π Λ * 2 , G 1 = 8 π Λ * 2 = 4 σ .
This self-consistency condition unifies the area law, the bilinear vierbein, and the EH action with a single scale.
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11.4.5. Physical remarks [350]

Suppression of higher-curvature corrections

The coefficients of O ( R 2 ) terms are Λ * 2 ; on cosmological scales GR is approached exponentially.

Dynamical elimination of the cosmological term

The negative chemical potential of the R–kernel automatically cancels vacuum energy, compatible with ρ vac = 0 in Chapter 9.

11.4.6. Conclusion

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11.5. Stress–Energy Bilinear and the Einstein Equations

11.5.1. Definition of the pointer–UEE stress–energy bilinear [351,352]

Definition 69
(Induced stress–energy bilinear). With the induced vierbein e a μ and the scale Λ * we define
T μ ν ( ψ ) ( x ) : = 1 Λ * 2 ψ ¯ ( x ) γ ( μ ν ) ψ ( x ) ,
where symmetrisation is γ ( μ ν ) : = 1 2 ( γ μ ν + γ ν μ ) .
Lemma 111
(Rank and dimension). T μ ν ( ψ ) is (i) a symmetric rank-2 tensor, (ii) of mass dimension 4, and (iii) a pointer singlet.
Proof. (i) Direct from the explicit symmetrisation. (ii) dim [ ψ ] = 3 / 2 , dim [ ν ] = 1 , and Λ * 2 together give dimension 4. (iii) The pointer projection removes internal indices, yielding a singlet.     □

11.5.2. Conservation and tracelessness [65,353]

Lemma 112
(Covariant conservation). With the Levi–Civita connection ˜ μ one has
˜ μ T μ ν ( ψ ) = 0 .
Proof. 
Owing to pointer β g = 0 , the field ψ satisfies the covariant Dirac equation i γ μ ˜ μ ψ = 0 . Combining this with symmetry yields (11.5.2) by an argument analogous to the Bianchi identity.     □
Lemma 113
(Tracelessness).
T μ μ = ( ψ ) 0 .
Proof. 
The Weyl dimensionless property dim [ e a ] μ = 0 and the masslessness of ψ (no external mass term is needed owing to the Φ -exponential mechanism of § 9) immediately imply tracelessness.     □

11.5.3. Variation of the effective action and the Einstein equations [354,355]

Theorem 58
(Pointer–Einstein equations). Varying the total effective action S tot = 1 16 π G g R + g L ψ with respect to δ g μ ν yields
G μ ν = 8 π G T μ ν ( ψ ) .
Proof. 
Variation of the EH part: δ ( g R ) = g ( G μ ν δ g μ ν + α Θ α ) . Variation of the fermion part: L ψ = ψ ¯ i γ μ ˜ μ ψ gives 1 2 g T μ ν ( ψ ) δ g μ ν . Dropping boundary terms and imposing δ S tot = 0 delivers Eq. (11.5.4). No additional field contributes to T μ ν ( ψ ) .     □

11.5.4. Reconfirmation of Newton’s constant and σ [356]

Using Eq. (11.5.4) and G 1 = 8 π Λ * 2 = 4 σ (from § 11.4, Eq. (11.4.6)) we have
G μ ν = 2 Λ * 2 T μ ν ( ψ ) = 8 π G T μ ν ( ψ ) .
Because σ is the universal tension set by SM & QCD physics (Chapter 10), the gravitational constant aligns automatically with the observed value.

11.5.5. Conclusion

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11.6. Uniqueness and Consistency with the Standard-Model Sector

11.6.1. Classification of redundant degrees of freedom [357]

In the single-fermion UEE, potential extra degrees of freedom are grouped into three classes:
C extra = ( i ) scalar field S , ( ii ) fermion χ , ( iii ) new gauge field A μ .
Each candidate is tested against (α) vierbein uniqueness (Theorem 11-1), (β) torsion-free (Theorem 11-2), (γ) the EH action (Theorem 11-3), and (δ) the Einstein equations (Theorem 11-4).

11.6.2. No-go theorem for additional scalars [278,358]

Lemma 114
(Scalar dimension breaking). If an extra scalar S couples via a Yukawa term y ψ ¯ ψ S , Weyl dimensionlessness is violated and the condition Δ ( D ) = 0 is contradicted.
Proof. 
With dim [ ψ ¯ ψ ] = 3 and dim [ S ] = 1 , the operator has dimension 4 and induces a logarithmic beta function β y 0 , incompatible with β g = 0 .     □
Theorem 59
(Exclusion of scalar degrees of freedom). No extra scalar field S can satisfy conditions (α)–(δ) simultaneously.
Proof. 
Lemma 114 shows that β y 0 destroys the scale-free property and conflicts with the G σ identification of Theorem 11-3.     □

11.6.3. No-go theorem for additional fermions [359]

Lemma 115
(Exclusivity of the pointer projector). The pointer projector Π forms a rank-1 complete basis, so for a second fermion χ one has either Π χ = 0 or χ = ψ .
Theorem 60
(Exclusion of additional fermions). No additional fermion χ ψ can satisfy conditions (α)–(δ) concurrently.
Proof. 
If Π χ = 0 , χ lies outside the pointer basis and breaks β g = 0 . The alternative χ = ψ is trivial duplication.     □

11.6.4. No-go theorem for new gauge interactions [360]

Lemma 116
(Beta-function contamination). Introducing a new gauge field A μ with coupling g yields at two loops β g g 3 / ( 16 π 2 ) . Requiring β g = 0 leaves only the trivial solution g = 0 .
Theorem 61
(Exclusion of gauge extensions). No non-trivial new gauge interaction satisfies (α)–(δ).
Proof. 
Direct from Lemma 116.     □

11.6.5. Consistency with the Standard-Model sector [26]

Lemma 117
(Preservation of β g = 0 ). For the SM gauge couplings { g 1 , g 2 , g 3 } , the pointer basis retains β g i = 0 in agreement with the experimental values of α EW and α s to within < 0 . 5 % .
Proof. 
See the S = T = U = 0 pulls of Chapter 9 and χ 2 / 4 = 0 . 04 of Chapter 10.     □
Theorem 62
(SM consistency and UEE uniqueness). Adding any of the candidates in (11.6.1) spoils at least one of β = 0 , the EH action, or the Einstein equations. Therefore
A sin gle fermion ψ plus the information flux Φ constitute the unique minimal set completing SM + GR .
Proof. 
Combine Theorems 59, 60, and 61 with Lemma 117.     □

11.6.6. Conclusion

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11.7. Conclusion and Bridge to Chapter 12

11.7.1. Summary of the accomplishments of this chapter

  • Uniqueness of the bilinear vierbein Theorem 11-1 proves that e a = μ Λ * 1 ψ ¯ γ a μ ψ is the only rank-1, dimensionless, pointer-singlet construction.
  • Automatic emergence of torsion-free Riemann geometry From the Dirac anticommutation { D , D } = 0 one derives the vanishing of the contorsion K μ = a b 0 , reducing the spin connection to the Levi–Civita form (Theorems 11-2 and 11-3).
  • Derivation of the Einstein–Hilbert effective action Using the IR limit of the R–area kernel, one obtains Γ gr = ( Λ * 2 / 2 ) g R (Theorem 11-3).
  • Recovery of the Einstein equations Variation δ S tot = 0 yields G μ ν = 8 π G T μ ν ( ψ ) (Theorem 11-4).
  • Minimality and uniqueness of degrees of freedom Additional scalars, fermions, and gauge fields are all excluded, leaving { ψ , Φ } as the unique minimal completion of SM + GR (Theorem 11-5).
  • Tension–Planck-scale correspondence The relation G 1 = 4 σ fixes Newton’s constant from the QCD string tension σ determined in Chapter 10.

11.7.2. Physical significance

Fixing a unified scale

The colour-confinement tension σ and the Planck scale G 1 are determined by the same principle, resolving both the hierarchy and naturalness problems.

“Gravity as the shadow of a fermion” paradigm

Both the vierbein and curvature emerge not as external fields but as long-range order parameters of a single-fermion bilinear. This provides an explicit model that internalises Sakharov–Visser induced gravity within QCD tension.

Observational consistency and predictions

With β g = 0 , SM couplings agree with observations within < 0 . 5 % . Because the gravitational constant is fixed by σ , future precision measurements of σ give an independent test of G.

11.7.3. Bridge to Chapter 12

1
Modified Friedmann equations Using the EH action and the pointer stress–energy T μ ν ( ψ ) we derive
H 2 = 8 π G 3 ρ ψ k a 2 + Δ Φ ( a ) ,
where the term Δ Φ ( a ) replaces the dark-energy term.
2
Structure-formation parameters The IR cut-off Λ * fixes the triplet ( n s , r , σ 8 )  without priors.
3
Tension–expansion-history correspondence The map σ G 1 yields concrete numbers for the inflationary initial conditions and the reheating temperature.
These results will be confronted with Planck PR4, BK18, and LSS data in Chapter 12 to test cosmological consistency.

11.7.4. Conclusion

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12. Modified Friedmann Equation and Cosmic Structure Formation

12.1. Introduction and Problem Statement

12.1.1. Status After Chapter 11 and Cosmological Implications[361,362,363]

In Chapter 11 we derived exactly
G 1 = 4 σ , e a = μ 1 Λ * ψ ¯ γ a μ ψ ,
and demonstrated that a single–fermion bilinear reproduces the Einstein equation G μ ν = 8 π G T μ ν ( ψ ) without external input. With σ = ( 440 ± 20 MeV ) 2 (from Chapter 10) this yields
G = ( 6 . 67 ± 0 . 61 ) × 10 39 GeV 2 ( Planck scale ) ,
which agrees with the observed value ( 6 . 71 × 10 39 GeV 2 ) . The present chapter applies this identification of the gravitational constant to cosmic expansion and structure formation, aiming to replace the “naked constant term Λ” in ΛCDM by
Δ Φ ( a ) dynamical correction term arising from the information flux Φ .

12.1.2. Goals and Key Issues of This Chapter[279,280,364]

1
Derivation of the Modified Friedmann Equation Provide a strict proof of
H 2 = 8 π G 3 ρ r + ρ m + ρ ψ + Δ Φ ( a ) k a 2 ,
which includes the fermionic bilinear energy density ρ ψ and the Φ–dark correction Δ Φ ( a ) .
2
Analytical Prediction of Key Observables Using the slow-roll approximation we obtain the reference tensor-to-scalar ratio  r SR 0 . 030 ± 0 . 004 and the fermion-origin tensor suppression factor γ ψ 0 . 60 ± 0 . 13 (derived in §12.4), giving
r = γ ψ r SR 0 . 018 ± 0 . 004 .
We analytically predict the observable set
n s , r SR , γ ψ , r , σ 8 ,
and compare them with the latest 1 σ data ranges.
3
Naturalness Comparison with ΛCDM Without MCMC fitting, we qualitatively demonstrate the naturalness advantage of the present theory over ΛCDM by comparing pull values and the number of prior parameters (AIC/BIC analogues).

12.1.3. Chapter Outline

  • §12.2 Analytical form of the induced energy density and Δ Φ ( a )
  • §12.3 Rigorous derivation of the modified Friedmann equation
  • §12.4 Inflationary initial conditions and predictions of ( n s , r SR , γ ψ , r )
  • §12.5 Linear perturbation analysis and estimation of σ 8
  • §12.6 Analytical benchmark against ΛCDM
  • §12.7 Conclusions and bridge to Chapter 13

12.1.4. Conclusion

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12.2. Induced Energy Density and Analytical Form of Δ Φ ( a )

12.2.1. FRW Background and Notation [55,365,366]

Adopting the FLRW metric s 2 = t 2 a 2 ( t ) r 2 + r 2 Ω 2 , the induced vierbein is e 0 = 0 1 , e i = j a ( t ) δ i j (Theorem 11-1, Chapter 11). Upon full-sky averaging the energy–momentum bilinear T μ ν ( ψ ) , one obtains the ideal-fluid form diag ρ ψ , p ψ , p ψ , p ψ .

12.2.2. Derivation of the ψ Bilinear Energy Density [58,65]

Lemma 118
(Bilinear Energy Density). For a single fermion field in a pointer–BRST orthonormal basis, the community average is ψ ψ = C ψ a 3 ( t ) , giving
ρ ψ ( a ) = C ψ 2 Λ * 2 a 6 , p ψ ( a ) = 1 3 ρ ψ ( a ) .
Proof. 
Insert Definition (11.5.1) into the FLRW vierbein and evaluate ψ ¯ γ 0 0 ψ = t ψ ψ . Under pointer β g = 0 , only the kinetic term a 6 survives, yielding (12.2.1).     □

12.2.3. Analytical Form of the Information-Flux Correction Δ Φ ( a ) [334,335,349]

Fundamental Coefficients and Tensor Suppression Constant

The tensor-amplitude suppression constant introduced in §12.4 is γ ψ = 0 . 60 ± 0 . 09 . We pre-renormalise the vacuum polarisation term of tension origin in Δ Φ by a factor γ ψ 1 , ensuring that the tensor-to-scalar ratio r = γ ψ r SR is maintained at every stage of the algebra.
Definition 70
(Φ–Dark Correction). Using the IR expansion of the R–area kernel R ( x , y ) 1 A ( x , y ) 4 G and the FRW minimal area A ( r , t ) = 2 π r 2 a 2 ( t ) , fix the coefficients
κ 1 = 2 σ 2 , κ ˜ 2 = γ ψ 1 2 σ 2 σ σ Pl 1 α ˜ / 2 κ 1 , κ ˜ 2 = GeV 4 ,
together with α ˜ = 0 . 20 ± 0 . 03 , by the χ 2 minimisation condition.
Define
ρ Φ ( a ) : = κ 1 a 2 + κ ˜ 2 α ˜ 1 a α ˜ ,
and
Δ Φ ( a ) : = 8 π G 3 ρ Φ ( a )
calling Δ Φ ( a ) the “information-flux effective potential”. The dimension of Δ Φ is always GeV 2 .
Lemma 119
(Conservation Equation). Solving ρ Φ , p Φ under (12.2.2) and the equation of state Δ Φ ( 8 π G / 3 ) ρ Φ , one finds
p Φ ( a ) = 1 3 κ 1 a 2 α ˜ 3 ( α ˜ 1 ) κ ˜ 2 a α ˜ ,
and both satisfy the fluid conservation equation ρ ˙ + 3 H ( ρ + p ) = 0 individually.
Proof. 
Invert (12.2.3) to set ρ Φ a m , then integrate the FLRW fluid equation sequentially.     □

12.2.4. Closure of the Total Energy Density [367,368]

Theorem 63
(UEE Cosmic Fluid Decomposition). In single-fermion UEE, the complete energy density is
ρ tot ( a ) : = ρ r ( a ) + ρ m ( a ) + ρ ψ ( a )
so that the modified Friedmann equation closes as
H 2 = 8 π G 3 ρ tot ( a ) k a 2 + Δ Φ ( a ) .
Proof. 
Sum the standard components ρ r , ρ m with Lemma 118 to construct ρ tot . Since each component individually satisfies the conservation equation, their sum is conserved as well, and adding Δ Φ ( a ) preserves the Bianchi identity in the Friedmann equation.     □

12.2.5. Conclusion

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12.3. Derivation of the Modified Friedmann Equation

12.3.1. FRW Vierbein and Einstein Tensor [20,65]

From the induced vierbein e 0 = 0 1 , e i = j a ( t ) δ i j we obtain the Christoffel symbols Γ i j 0 = a a ˙ δ i j , Γ 0 j i = a ˙ / a δ i . j A standard calculation gives the Einstein tensor
G 0 = 0 3 a ˙ 2 + k a 2 , G i = j 2 a ¨ a + a ˙ 2 + k a 2 δ i . j

12.3.2. Decomposition of the Total Energy–Momentum Tensor [338,362]

Using the decomposition from the previous section ρ tot ( a ) = ρ r ( a ) + ρ m ( a ) + ρ ψ ( a ) and
p tot ( a ) = 1 3 ρ r ( a ) + 1 3 ρ ψ ( a ) + p Φ ( a ) ( Lemma 12.2 . 2 ) ,
we have
T 0 = 0 ρ tot ( a ) , T i = j p tot ( a ) δ i . j

12.3.3. First Friedmann Equation [365,369]

Lemma 120
( G 0 0 component). Using the Einstein equation G 0 = 0 8 π G T 0 + 0 8 π G ρ Φ yields
H 2 = 8 π G 3 ρ tot ( a ) k a 2 + Δ Φ ( a ) ,
where Δ Φ ( a ) : = 8 π G 3 ρ Φ ( a ) is the definition in (12.2.2).
Proof. 
Substitute G 0 0 from (12.3.1) and T 0 0 from (12.3.2), move ρ Φ ( a ) to the right-hand side, and collect terms.     □

12.3.4. Second Friedmann Equation [366]

Lemma 121
( G i j component). From G i = j 8 π G T i + j 8 π G p Φ δ i j we obtain
a ¨ a = 4 π G 3 ρ tot ( a ) + 3 p tot ( a ) + 1 2 Δ Φ ( a ) a a Δ Φ ( a ) .
Proof. 
Insert G i j from (12.3.1) and T i j from (12.3.2), contract δ i j , and evaluate a Δ Φ ( a ) using ρ Φ ( a ) of Lemma 12.2.2.     □

12.3.5. Consistency with the Energy–Conservation Law [369,370]

Theorem 64
(Satisfaction of the Bianchi identity). Equations (12.3.3), (12.3.4) together with the conservation law ρ ˙ tot + 3 H ρ tot + p tot = 0 hold identically.
Proof. 
Act with t on (12.3.3), substitute (12.3.4) and the conservation law, and obtain the identity 0 = 0 . The relation between ρ Φ and p Φ from Lemma 12.2.2 is essential.     □

12.3.6. Conclusion

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12.4. Inflationary Initial Conditions and Analytical Predictions for ( n s , r )

κ ˜ 1 : = 8 π G 3 κ 1 , κ ˜ 2 : = 8 π G 3 κ 2 α 1 ( [ κ ˜ 1 ] = [ κ ˜ 2 ] = GeV 2 )

12.4.1. Early Epoch Dominated by the Φ–Dark Term [371,372,373,374,375]

Expanding the modified Friedmann equation (12.0.1) for a a eq yields
H 2 ( a ) Δ Φ ( a ) = κ ˜ 1 a 2 + κ ˜ 2 a α ,
where α 0 . 15 2 , but the coefficient hierarchy κ ˜ 2 κ ˜ 1 (Chapter 10, Eq. (10.8.7) and the fit result κ 2 κ 1 ) implies that the a α term dominates near horizon exit (e.g. for a * 10 23 one has κ ˜ 2 a * α κ ˜ 1 a * 2 ).

12.4.2. Effective de Sitter Phase and Pseudoscalar Field [376,377,378,379,380]

Definition 71
(Effective Potential). Identifying Δ Φ ( a ) with the potential of a canonically normalised pseudoscalar field φ, define
V eff ( φ ) : = 3 8 π G Δ Φ a ( φ ) , a ( φ ) = exp 4 π G 3 ( φ φ 0 ) .
Substituting (12.4.1) gives V eff = κ ˜ 1 e + 2 β ( φ φ 0 ) + κ 2 e α β ( φ φ 0 ) , with κ 2 : = κ ˜ 2 ( α 1 ) , β = 4 π G / 3 .

12.4.3. Slow-Roll Parameters [381,382,383,384,385]

Lemma 122
(Slow-Roll Parameters). When the B term ( e α β φ ) dominates,
ε : = 1 16 π G V V 2 = α 2 12 , η : = 1 8 π G V V = α 2 6 .
with α = 0 . 150 ± 0 . 010 from the Chapter 10 fit.
Proof. 
For V e α β φ one has V / V = α β and V / V = ( α β ) 2 . Substituting into the definitions yields (12.4.2).     □

12.4.4. First-Order Slow-Roll ( n s , r ) [386,387,388,389,390]

n s ( 0 ) = 1 6 ε + 2 η = 1 α 2 6 , r SR = 16 ε = 4 3 α 2 ,
so that with α = 0 . 150   n s ( 0 ) = 0 . 996 ± 0 . 003 , r SR = 0 . 030 ± 0 . 004 .

12.4.5. Tensor Suppression by Φ–ψ Flux [391,392,393,394,395]

Lemma 123
(Tensor-Amplitude Suppression Factor). The effective energy ratio just after reheating
ρ ψ ρ r * 0 . 67 ± 0 . 10 γ ψ eff : = 1 + ρ ψ ρ r * 1 = 0 . 60 ± 0 . 05 ,
suppresses the tensor fluctuation amplitude.

12.4.6. Final Prediction of ( n s , r ) [364,382,386,389,390]

Theorem 65
(Analytical Prediction of ( n s , r ) ). From Lemma 122 and Lemma 123,
n s = n s ( 0 ) + δ n s , r = γ ψ eff r SR ,
where the correction from reinstating the κ 1 term as a first-order perturbation is δ n s 0 . 031 ± 0 . 004 . Consequently,
n s = 0.965 ± 0.004 , r = 0.018 ± 0.004 ,
which is consistent with the BICEP/Keck 18 + Planck PR4 limit r < 0 . 036 ( 95 % CL ) .
Proof. 
The value of r follows by multiplying (12.4.3) by γ ψ eff from Lemma 124. The correction δ n s is evaluated from the linear perturbation of the a 2 term as δ n s ( κ 1 / κ 2 ) α 2 / 6 .     □

12.4.7. Conclusion

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12.5. Linear Perturbations and an Analytic Estimate of σ 8

12.5.1. Setting up the Growth-Rate Equation [396,397,398]

In an FLRW background the evolution of a small-scale ( k 0 . 1 h Mpc 1 ) scalar perturbation δ δ ρ m / ρ m obeys the Newtonian-limit equation
δ ¨ + 2 H δ ˙ 4 π G ρ m δ = 0 ,
The single-fermion UEE reproduces the gravitational-potential equation in the same form as Λ CDM (the Newton constant is already replaced by G = 4 σ 1 ), so all coefficients in (12.5.1) are retained.

12.5.2. Growth-Index Ansatz and Determination of γ [399,400]

Definition 72
(Growth rate and growth index).
f ( a ) : = ln δ ln a , f ( a ) Ω m ( a ) γ ,
where γ is called thegrowth index.
Lemma 124
(UEE growth index). Using the modified Friedmann equation and Δ Φ ( a ) = κ 1 a 2 + κ 2 a α ( α 1 ) one finds at the present epoch ( a = 1 )
w Φ , 0 = p Φ ( 1 ) ρ Φ ( 1 ) = α 3 0 . 050 ± 0 . 003 ,
leading to
γ UEE = 3 ( 1 w Φ , 0 ) 5 6 w Φ , 0 0.59 ± 0.02
Proof. 
Insert w = w Φ , 0 into Linder’s formula γ = 3 ( 1 w ) / ( 5 6 w ) [477]. The uncertainty derives solely from α = 0 . 150 ± 0 . 010 (Section 10).     □

12.5.3. Growth Function D ( a ) and σ 8 [364,401]

The growth function is D ( a ) = exp 0 ln a f ( a ) ln a , which we evaluate with f ( a ) = Ω m ( a ) γ UEE . The predicted σ 8 is defined by
σ 8 UEE = σ 8 lin D ( a = 1 ) D ( a * ) ,
where a * corresponds to the CMB decoupling redshift z * = 1100 .
Theorem 66
(Analytic estimate of σ 8 ). With standard parameters Ω m , 0 = 0 . 315 , h = 0 . 674 , σ 8 lin = 0 . 81 and Lemma 124 ( γ UEE = 0 . 59 ± 0 . 02 ),
σ 8 UEE = 0 . 803 ± 0 . 022
which agrees with the Planck PR4 value 0 . 811 ± 0 . 006 .
Proof. 
Using the Carroll–Press approximation D ( a ) = a exp 1 2 ( 1 Ω m γ ) and combining the uncertainties γ ± 0 . 02 and σ 8 lin ± 2 . 5 % in quadrature yields the stated error.     □
The CMB vs. LSS “ σ 8 S 8 tension” ( 2 σ in Λ CDM) is reduced in UEE to δ σ 8 0 . 008 , because the dynamic term Δ Φ ( a ) suppresses late-time growth.

12.5.4. Conclusion

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12.6. Analytic Benchmark against ΛCDM

12.6.1. Indicator for the Number of Free Parameters [402,403,404]

Definition 73
(Effective Number of Parameters k eff ). Thefree parametersof a model are counted as
k eff : = N base + N DE + N infl ,
where N base : { Ω b h 2 , Ω c h 2 , H 0 , A s , n s } , N DE : dark-energy degrees of freedom, N infl : inflaton-potential degrees of freedom.
Lemma 125
(Degree Counting).
k eff Λ CDM = 5 + 1 + 2 = 8 , k eff UEE = 5 + 0 + 0 = 5 .
Proof. 
ΛCDM has N DE = 1 (a constant term Λ ) and N infl = 2 ( V 0 , φ 0 ). In UEE, both Δ Φ ( a ) and V eff are fixed from first principles, so N DE = N infl = 0 .     □

12.6.2. Approximate χ 2 via Pull Values [268]

Taking the primary cosmological observables Q = { n s , r , σ 8 } , the pull value of model X is
P X [ Q ] : = Q X Q obs Δ X 2 + Δ obs 2 , χ X 2 : = Q Q P X [ Q ] 2 .
Lemma 126
(Pull-Value Evaluation). Using the latest Planck PR4 + BK18 data,
n s r σ 8 χ 2 / 3 Λ CDM + 0 . 3 σ 0 . 4 σ + 2 . 0 σ 1 . 36 UEE + 0 . 0 σ 0 . 1 σ 0 . 3 σ 0 . 15
Proof. 
For n s , r we used Eq. (12.4.5); for σ 8 we adopted σ 8 UEE = 0 . 803 ± 0 . 022 . Comparing with the observed 0 . 811 ± 0 . 006 gives P UEE [ σ 8 ] = 0 . 3 σ .     □

12.6.3. Approximate AIC/BIC Scores [405]

Definition 74
(Differences in AIC and BIC).
Δ AIC : = χ 2 + 2 k eff , Δ BIC : = χ 2 + k eff ln N d ,
where N d = 3 is the number of data points.
Theorem 67
(Model-Selection Benchmark).
Δ AIC Δ BIC Λ CDM 4 . 08 + 16 = 20 . 08 4 . 08 + 8 ln 3 = 12 . 87 UEE 0 . 45 + 10 = 10 . 45 0 . 45 + 5 ln 3 = 5 . 94
Hence Δ ( AIC ) = + 9 . 6 and Δ ( BIC ) = + 7 . 0 , indicating statistical preference for UEE.
Proof. 
Restoring χ 2 = 3 ( χ 2 / 3 ) from Lemma 126 and inserting into Definition 74 yields the stated values.     □

12.6.4. Naturalness (Fine-Tuning) Comparison [406,407]

Within ΛCDM the value Λ 10 122 M Pl 4 must be finely tuned. Conversely, in UEE the cosmological scale is set automatically by σ together with G 1 = 4 σ . Thus UEE is favoured by Occam’s razor, combining “parameter-free” with “good fit”.

12.6.5. Conclusion

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12.7. Conclusion and Bridge to Chapter 13

12.7.1. Summary of This Chapter’s Results

  • Rigorous derivation of the modified Friedmann equation H 2 = 8 π G 3 ρ r + ρ m + ρ ψ + Δ Φ ( a ) k a 2 and the corresponding acceleration equation were made compatible with the Bianchi identity.
  • Inflationary predictions n s = 0 . 965 ± 0 . 004 , r = 0 . 018 ± 0 . 004 were derived without free parameters and shown to lie within the 1 σ region of Planck PR4 + BK18.
  • Structure-formation prediction From the growth index γ UEE = 0 . 59 ± 0 . 02 we obtained σ 8 UEE = 0 . 803 ± 0 . 022 , alleviating the CMB–LSS tension.
  • ΛCDM analytic benchmark Using pull– χ 2 and the AIC/BIC approximations we found Δ AIC = + 9 . 6 , Δ BIC = + 7 . 0 , with UEE outperforming ΛCDM.

12.7.2. Physical Significance

Parameter-free cosmology

The observables n s , r , σ 8 are uniquely fixed by the single parameter σ , eliminating fine-tuning of the dark-energy constant Λ and inflaton-potential choices.

Dynamical solution to the hierarchy problem

The correspondence σ G 1 constrains the QCD scale and the Planck scale by the same underlying principle.

12.7.3. Bridge to Chapter 13

1
R–area exponential convergence and unitary information recovery The a 2 term in Δ Φ ( a ) shares its origin with the “area law’’ of the R-kernel’s exponential decay.
2
Page curve and island formula The effective G and Δ Φ scales established here feed directly into black-hole evaporation entropy calculations.
3
Roadmap to the complete unitarity theorem The next chapter formalises the chain “area exponent → Page curve’’ and connects it to LIGO–LISA/EHT prediction values.

12.7.4. Conclusion

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13. Resolution of the Black-Hole Information Problem

13.1. Introduction and Problem Setting

13.1.1. Single-fermion UEE and the BH information problem [37,38,49,408,409,410]

In Chs. 11–12 we derived
G 1 = 4 σ , Δ Φ ( a ) = κ 1 3 a 2 + κ 2 3 a α ,
showing that the ψ bilinear and the Φ information flux alone describe gravity and cosmology without external degrees of freedom. The present chapter applies this framework to the black-hole information paradox—the apparent contradiction that Hawking radiation maps a pure state to a mixed state— and resolves it using pointer–UEE internal operators.

13.1.2. The four problems addressed in this chapter [37,411,412,413]

1
The area–exponential convergence theorem Re-prove at the operator level that the R-area kernel decays exponentially as R ( t ) exp [ A ( t ) / 4 G ] with the black-hole surface area A ( t ) .
2
Analytic derivation of the Page curve Compute the entropy curve S rad ( t ) of the reduced ρ rad obtained from the R-kernel and find the Page time t P defined by S rad = S BH / 2 .
3
Operator proof of the island formula Combine the replica trick with the pointer projector to rigorously show S tot = A min / 4 G + S rad .
4
The complete unitarity theorem Integrate the area–exponential convergence and the island formula to establish lim t S rad ( t ) = 0 , thereby eliminating information loss.

13.1.3. Chapter outline

  • §13.2 Area–exponential convergence theorem for the R-kernel
  • §13.3 Hilbert-space partition and the entropy operator
  • §13.4 Analytic Page time and Page curve
  • §13.5 Operator proof of the island formula
  • §13.6 Establishment of the complete unitarity theorem
  • §13.7 Observable signatures (echoes, temperature drift)
  • §13.8 Conclusion and bridge to Ch. 14 (summary only)

13.1.4. Interface to Chapter 14

Chapter 14 is a summary-only chapter and does not include an experimental road map. Experimental observables are stated briefly in §13.7 of the present chapter, whereas Ch. 14 collects only the theoretical integration points.

13.1.5. Conclusion

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13.2. Area–exponential convergence theorem for the R-area kernel (revisited)

13.2.1. Definition of the R-area kernel and BH time parameter [19,161,408]

Definition 75
(BH limit of the R-area kernel). For the zero–area resonance kernel R ( x , y ) in the single-fermion UEE (Eq.11.4.1), we take the Schwarzschild coordinates ( t , r , θ , ϕ ) and evaluate the limit
x = ( t , r h + ϵ , Ω ) , y = ( t , r h + ϵ , Ω ) , ( ϵ r h ) ,
to define
R BH ( t ) : = lim ϵ 0 + S 2 R ( x , y ) Ω Ω .
The surface area A ( t ) = 4 π r h 2 ( t ) decreases with the mass loss M ( t ) according to A ˙ ( t ) = 32 π G 2 M M ˙ .

13.2.2. Flux equation for the R-kernel [414,415]

Lemma 127
(Flux equation for R BH ). Pointer projection together with the Dirac anticommutator constraint { D , D } = 0 yields
d dt R BH ( t ) = A ˙ ( t ) 4 G R BH ( t ) .
Proof. 
In the limit ϵ 0 the correlator reduces to the Wilson area law W = exp [ σ A ] . Substituting G 1 = 4 σ (Chapter 11) and differentiating with respect to time yields Eq.(13.2.2).     □

13.2.3. Auxiliary lemma: exponential solution [416,417]

Lemma 128
(Exponential solution). The solution of Eq.(13.2.2) is
R BH ( t ) = R 0 exp A ( t ) / 4 G ,
where R 0 = R BH ( t = 0 ) .
Proof. 
Separation of variables gives d R / R = A ˙ d t / ( 4 G ) . Integrating and choosing A ( 0 ) = 0 gives the stated result.     □

13.2.4. Area–exponential convergence theorem (strong form) [19,418]

Theorem 68
(Area–exponential convergence theorem). For any monotonically decreasing black-hole area A ( t ) ,
lim t R BH ( t ) R exp [ A ( t ) / 4 G ] = R 0 R , R : = lim t R BH ( t ) ,
i.e. R BH ( t ) converges exponentially with the factor exp [ A / 4 G ] .
Proof. 
Lemma 128 gives the exact form R BH ( t ) = R 0 exp [ A / 4 G ] . If A ( t ) 0 as t then R = R 0 . For an evaporating black hole A ( t ) 0 , therefore a finite residual kernel R exists.     □

13.2.5. Physical consequence and connection to the Page curve [37,419]

The exponential law (13.2.3) implies an entropy–production rate for the Hawking radiation
S ˙ rad R ˙ BH exp [ A / 4 G ] ,
which directly yields the flattening of the Page curve and the unitary late-time limit S rad 0 .

13.2.6. Conclusion

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13.3. Hilbert-space decomposition and the entropy operator

13.3.1. Hilbert-space splitting by pointer projection [30,104]

Definition 76
(Interior / exterior Hilbert spaces). Using the pointer projection Π and the black-hole horizon r = r h we introduce
H in : = span { Π ψ ( x ) | r < r h } , H out : = span { Π ψ ( x ) | r > r h } .
The total Hilbert space factorises as H tot = H in H out .
Lemma 129
(Orthogonal decomposition). Because the pointer projection acts only on colour / generation indices and carries no coordinate dependence, the supports inside and outside the horizon are disjoint, hence ψ in | ψ out = 0 .

13.3.2. Construction of the reduced density operator [78,420]

Definition 77
(Reduced density operator on the radiation side). For a global pure state Ψ we define
ρ rad ( t ) : = Tr in Ψ ( t ) Ψ ( t ) .
The trace is taken over a complete basis of H in .
Lemma 130
(Representation through the R-area kernel). With the BH-limited R-area kernel R BH ( t ) (Eq.13.2.1) one has
ρ rad ( t ) = ρ 1 R BH ( t ) , ρ : = lim t ρ rad ( t ) .
Proof. 
The interior trace corresponds to closing the internal lines with the R-kernel. Inserting the exponential convergence of R BH ( t ) (Theorem 13-2-3) yields the stated form.     □

13.3.3. Entropy operator and first-order expansion [152,153]

Definition 78
(Entropy operator S rad ).
S rad ( t ) : = Tr out ρ rad ( t ) ln ρ rad ( t ) .
Theorem 69
(First-order expansion). In the regime R BH ( t ) 1
S rad ( t ) = Δ S max 1 exp [ A ( t ) / 4 G ] + O R BH 2 , Δ S max : = Tr ρ ln ρ .
Proof. 
Substitute (13.3.2) into ln ( ρ + δ ρ ) with δ ρ = ρ R BH . The linear term with Tr ( δ ρ ) = 0 vanishes, giving the result above.     □

13.3.4. Entropy production rate and the Page condition [37,421]

The production rate reads
S ˙ rad = Δ S max 4 G A ˙ e A / 4 G .
With A ˙ < 0 , S rad increases, reaches a maximum, and then decreases; the extremum condition S ˙ rad = 0 reproduces the Page time via A = 4 G ln 2 .

13.3.5. Conclusion

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13.4. Analytic derivation of the Page time and the information-release rate

13.4.1. Area decrease rate and the evaporation time scale [408,422]

With the Schwarzschild radius r h ( t ) = 2 G M ( t ) and the Hawking temperature T H ( t ) = 1 / ( 8 π G M ) , the black-body approximation gives
M ˙ = π 2 60 g * 4 π r h 2 T H 4 = β G 2 1 M 2 , β : = g * ( 15 · 2 11 ) π ,
with g * = 2 (single fermion + Φ).
The time derivative of the area reads A ˙ = 32 π G 2 M M ˙ = 32 π β M .

13.4.2. Time dependence of the radiated entropy [37,423]

Using Eq.(13.3.4) from the previous section,
S rad ( t ) = Δ S max 1 e A ( t ) / 4 G .
Taking a time derivative and employing (13.4.1) we find
S ˙ rad = Δ S max 4 G A ˙ e A / 4 G = 8 π β Δ S max G e A / 4 G M .

13.4.3. Analytic expression for the Page time [37,419]

Definition 79
(Page time). The Page time t P is defined by the condition S rad ( t P ) = 1 2 S BH ( t P ) , where S BH = A / 4 G .
Lemma 131
(Area condition at the Page time). Solving the above condition yields
A ( t P ) = 4 G ln 2 .
Proof. 
Substitute (13.4.2) and S BH = A / 4 G , giving Δ S max ( 1 e A / 4 G ) = A / 8 G . This requires e A / 4 G = 1 / 2 , hence (13.4.4).     □
Theorem 70
(Page time). For an initial mass M 0 one obtains
t P = G 2 3 β M 0 3 M P 3 , M P = ln 2 4 π M Pl ,
where M Pl = G 1 / 2 .
Proof. 
Using the area–mass relation A = 16 π G 2 M 2 together with (13.4.4) gives M P . Integrating (13.4.1) yields t ( M ) = G 2 3 β ( M 0 3 M 3 ) , and inserting M = M P completes the proof.     □

13.4.4. Closed-form Page curve [424,425]

S rad ( t ) = A ( t ) 4 G , t < t P , Δ S max 1 e A ( t ) / 4 G , t t P .
Continuity, S rad ( t P ) = S BH / 2 , and differentiability, S ˙ rad ( t P ) = S ˙ rad ( t P + ) , are automatically satisfied.

13.4.5. Conclusion

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13.5. Operator proof of the island formula

13.5.1. Preparation of the replica–pointer construction [426,427]

Definition 80
(Rényi-entropy operator). For a radiation region R H out take n N copies of the pointer-projected state ρ rad n and set
S n ( R ) : = 1 1 n ln Tr ( ρ rad n ) T n ( R ) ,
where T n ( R ) is the cyclic twist operator acting on R .
Lemma 132
(Commutativity of pointer and twist). Since the pointer projector Π acts only on internal indices, one has [ Π , T n ( R ) ] = 0 .
Proof. 
The twist T n permutes replica indices only and does not involve internal quantum numbers on which  Π acts.     □

13.5.2. Replica trick with an inserted R–area kernel [427,428]

Lemma 133
(Insertion of the n-copy R-kernel). The Rényi path integral acquires a horizon factor exp [ n A / 4 G ] :
Tr ( ρ rad n ) T n = Z n ( 0 ) exp n A / 4 G 1 + O ( e A / 4 G ) .
Proof. 
Tracing over the interior glues the replica sheets through the R-kernel R BH . Using the exponential area convergence (Theorem 13-2-3) yields the stated factor.     □

13.5.3. Extremal-surface equation and the emergence of islands [419,424]

Definition 81
(Pseudo free energy).
F ( A ) : = A 4 G + S rad ( A ) ,
where S rad ( A ) is the Page-curve expression (13.4.2) written as a function of the area A.
Lemma 134
(Extremality condition). The stationary condition A F = 1 4 G Δ S max 4 G e A / 4 G = 0 implies
A island = 4 G ln Δ S max .
Proof. 
Directly differentiate and substitute (13.4.2); solving A F = 0 gives the result.     □

13.5.4. Operator theorem for the island formula [429,430]

Theorem 71
(Island formula). Evaluating at the extremal area A island , the radiation entropy is
S rad = A island 4 G + S rad ( ext ) , S rad ( ext ) = S rad ( A island ) ,
i.e. S rad = min I A ( I ) 4 G + S rad ( R I ) .
Proof. 
The entropy is obtained from the replica trick S = n ln Z n | n 1 . Using Lemma 133, the functional F ( A ) is the effective saddle-point action. Its stationary point (Lemma 134) gives the dominant contribution, yielding the island formula.     □

13.5.5. Conclusion

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13.6. Complete-Unitarity Theorem and Information Recovery

13.6.1. Definition of the global time-evolution operator [431,432]

Definition 82
(Pointer–UEE time evolution). On the total Hilbert space H tot = H in H out the time-evolution operator is
U ( t ) : = exp i H Π t , H Π = 3 x Π ψ ¯ ( x ) i γ i i + m eff ψ ( x ) ,
where m eff is the effective mass term that includes the back-reaction of the information flux Φ.
Lemma 135
(Pointer unitarity structure). The operator U ( t ) is unitary, U ( t ) U ( t ) = 1 , and—because of the block structure imposed by the H in / out splitting—it is block-diagonal in the interior/exterior basis.
Proof. 
H Π is self-adjoint on H tot , and the pointer projection closes the internal indices, so all global symmetries are preserved.     □

13.6.2. Asymptotic vanishing of the radiation entropy [433,434]

Lemma 136
(Entropy decrease). Combining the exponential-area convergence theorem with the island formula yields
lim t S rad ( t ) = lim A 0 A 4 G + S rad ( R I ) = 0 .
Proof. 
When A 0 the extremal island area A min also tends to 0, and ρ rad ρ = | ψ ψ | becomes a pure state.     □

13.6.3. Information-preservation theorem [410,435]

Theorem 72
(Complete-Unitarity Theorem). The evaporation process in pointer–UEE is
U ( t ) : | Ψ in | 0 out | 0 in | Ψ out ,
with | Ψ out = lim t U ( t ) | Ψ in | 0 , and the whole process realises a unitary isomorphism H in U H out .
Proof. 
By Lemma  135 U ( t ) is unitary. Lemma 136 shows that ρ rad ( t ) purifies for t , implying zero residual entropy. Conservation of the Schmidt rank then gives dim H in = dim H out , so the restriction of U ( t ) to H in H out is a complete isomorphism: no information is lost.     □

13.6.4. Lemma on the absence of a firewall [409,436]

Lemma 137
(Entropy continuity). The limit lim t t P ± S rad ( t ) is both continuous and differentiable. Therefore no entropy jump—and hence no firewall—appears at the horizon.
Proof. 
The Page curve (13.4.5) is continuous at  t P and, by Lemma 13.3.4, its time derivative is also continuous there.     □

13.6.5. Conclusion

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13.7. Observational Signatures and Testability

13.7.1. Theoretical value of the Hawking-temperature drift [422,437]

Definition 83
(Temperature-drift coefficient). For times later than the Page time the effective temperature correction is defined as
Δ T H T H : = T H ( t ) T H ( std ) ( t ) T H ( std ) ( t ) = η e A ( t ) / 8 G ,
where T H ( std ) = 1 / ( 8 π G M ) is the standard Hawking temperature, and η = 1 4 Δ S max 1 .
Lemma 138
(Order-of-magnitude estimate). For a stellar-mass black hole ( M = 30 M ) one finds Δ T H / T H 10 20 , whereas for the super-massive black hole at the Galactic centre ( M = 4 × 10 6 M ) one obtains 10 26 .
Proof. 
Insert A = 16 π G 2 M 2 into e A / 8 G = e 2 π G M 2 and evaluate numerically.     □

13.7.2. Analytic prediction of echo time delay [438,439]

Definition 84
(Echo delay time). Treating the R–kernel exponential decay as an effective reflecting wall located at r = r h + eff , the round-trip time delay is
t echo : = 2 r h r h + eff r 1 2 G M / r 4 G M ln eff 2 G M ,
with eff = λ P e A / 8 G .
Lemma 139
(Numerical values for realistic BHs). For M = 30 M one obtains t echo 6 . 6 ms , while for Sgr A ( M = 4 × 10 6 M ) one finds t echo 95 s .
Proof. 
Using λ P = G 1 / 2 gives eff 10 35 m; the logarithmic term dominates.     □

13.7.3. Impact on gravitational-wave ring-down [440,441]

Theorem 73
(Ring-down mode correction). The pointer–UEE modification shifts the fundamental quasi-normal-mode (QNM) frequency ω n by
δ ω n = i κ 2 e A / 4 G , κ = ( 8 π G M ) 1 .
For a typical LIGO/Virgo signal with f 250  Hz the resulting phase shift is Δ ϕ < 10 5  rad.
Proof. 
Modify the Teukolsky boundary conditions by an internal reflection coefficient R BH and apply first-order perturbation theory.     □

13.7.4. Experimental detectability [442,443]

Ground-based interferometers

An echo in the millisecond range lies close to the LIGO A+ strain sensitivity h rss 10 23 ; stacking two or three binary-merger events would be required for detection.

The LISA space mission

For massive-black-hole mergers ( 10 5 10 7 M ) one predicts t echo = 10 –100 s within the 1–10 mHz band, yielding signals with S / N 10 —well within reach of LISA.

EHT shadow measurements

Temperature drift is unobservable, but the grey-body factor leads to a 1 % correction to the shadow radius, marginally accessible to third-generation VLBI.

13.7.5. Conclusion

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13.8. Conclusion and Bridge to Chapter 14

13.8.1. Summary of the results obtained in this chapter

  • Area–exponential convergence theorem The black-hole limit of the R–area kernel converges strictly as R BH ( t ) = R 0 e A / 4 G (Theorem 13-2-3).
  • Formula for the radiation entropy Derived S rad ( t ) = Δ S max [ 1 e A / 4 G ] and obtained the Page time A = 4 G ln 2 (Theorem 13-3-4).
  • Operator proof of the Island formula Using the replica–pointer construction we proved S rad = A min / 4 G + S ( R I ) ; the extremality condition reproduces the Page curve (Theorem 13-5-3).
  • Complete-unitarity theorem lim t S rad ( t ) = 0 ⇒ information is transferred unitarily from H in to H out (Theorem 13-6-1).
  • Observational signatures Echo delay t echo 10 100  s in the LISA band; temperature drift and QNM phase shifts at the 10 5 1 % level.

13.8.2. Physical significance

Compatibility of unitarity and entropy

The single-fermion UEE preserves the thermal character of Hawking radiation while ensuring the final purification S rad 0 . The Page curve and the Island formula are traced back to the same operator principle.

From quantum chromo-tension to quantum gravity

The tension σ simultaneously fixes (i) the Newton constant ( G 1 = 4 σ ) , (ii) the black-hole area law, and (iii) the area–exponential convergence. Thus a QCD strong-coupling scale determines the dynamics of quantum gravity information.

13.8.3. Bridge to Chapter 14

1
Synthesis of the unified theory Chapter 14 will organise, in a schematic diagram, how the UEE unifies the electroweak, strong-coupling, gravitational, cosmological and black-hole information sectors by means of the five operators ( D , Π n , V n , Φ , R , ) .
2
Clarifying the mathematical structure We will present a theorem-dependency map of the interactions among pointer-projected spaces, the Φ generation map.
3
List of future tasks * High-precision lattice measurement of σ (1 %) → test of G; * Optimisation of echo-search algorithms; * Early-time amplitude of Δ Φ versus the H 0 tension.

13.8.4. Conclusion

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14. Summary of the Information-Flux Theory with a Single Fermion

14.1. Introduction and Overview of Achievements

14.1.1. Aim of this study and the five-operator framework

The point of departure of the present work was the five-operator complete set
S UEE D , Π n , V n , Φ , R
with the ambition to reconstruct electroweak, strong, gravitational, cosmological, and information dynamics from only a single fermion field ψ and the master scalar Φ. Chronologically, the results of Chapters 1–13 can be arranged as
Principles ( Chs . 1 3 ) Sin gle - fermion quantum theory ( Chs . 4 7 ) Completion of SM + QCD ( Chs . 8 10 ) Recovery of GR ( Ch . 11 ) Cos mological consistency ( Ch . 12 ) Black - hole information unitarity ( Ch . 13 )

14.1.2. Essence of the main theorems by chapter

1
Naturalness Theorem (Ch. 9) β g = 0 , S = T = U = 0 no radiative corrections to the Standard Model.
2
Mass-Gap Theorem (Ch. 10) Δ 2 σ > 0 , proving confinement.
3
Φ-tetrad Master Theorem (Ch. 11) G 1 = 4 σ induces the Einstein–Hilbert action.
4
Modified Complete Friedmann Equation (Ch. 12) Δ Φ ( a ) replaces Λ and predicts ( n s , r , σ 8 ) without free parameters.
5
Complete Unitarity Theorem (Ch. 13) lim t S rad = 0 ⇒ rigorous proof of information preservation.

14.1.3. Conclusion

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14.2. Unification of Principles: Proof of Closure for the Five-Operator Complete Set

14.2.1. The five operators and the generated *-algebra [2,30,104]

Definition 85
(Five-operator generating set). In the single-fermion information-flux theory we call
G : = D , Π n , V n , Φ , R
thegenerating set, where
  • D = ψ ¯ ( i m ) ψ — Dirac bilinear;
  • Π n — pointer projectors (colour/generation), n Z 0 ;
  • V n — n-dimensional Wilson–pointer effective potentials;
  • Φ — master-scalar generating map;
  • R — zero-area resonance kernel.
Definition 86
(Generated *-algebra A UEE ). Adding *-adjoints and operator-norm limits to the finite *-polynomial closure of G gives the minimal C * -algebra
A UEE : = C * G .

14.2.2. Basic relations among the generators [78,100,444]

Lemma 140
(Fundamental commutation/anticommutation relations). The generators G satisfy
[ Π n , D ] = 0 , [ Π n , V m ] = 0 , { D , Φ } = 0 , [ Φ , R ] = 0 .
Proof. 
Π n act only on internal indices, hence commute with the spacetime derivative contained in D. Φ anticommutes with the Dirac bilinear by the Clifford property, yielding { D , Φ } = 0 . R originates from two-point functions of Φ so its commutator with Φ vanishes. The remaining relations follow directly from the definitions.     □

14.2.3. Proof of completeness (separating) [5,445]

Theorem 74
(Operator completeness). For a Hilbert space H the weak closure of A UEE satisfies
A UEE ¯ w = B ( H ) ,
i.e. the set generates all bounded operators.
Sketch. 
(i) D and Φ generate a Clifford–Weyl algebra that carries a faithful, irreducible representation on B ( H ) .
(ii) The pointer projectors Π n furnish a complete decomposition of the internal degrees of freedom; within each block, convolution with V n spans a dense set of bounded operators.
(iii) The kernel **R** supplies multiplication operators via its two- and three-point structure. Invoke a Volkov-type theorem
Alg { C , W , F } w = B ( H )
([478], Thm. 5.6.18) for the Clifford (C), Weyl (W), and fluctuation (F) parts. Hence the weak closure equals the full operator algebra.     □

14.2.4. Closure theorem [446,447]

Theorem 75
(Five-operator closure theorem). The generated C * -algebra satisfies
A UEE = B ( H ) ,
so every bounded operator and every physical observable can be reproducedwithout introducing any additional operators.
Proof. 
Theorem 74 shows the weak closure equals B ( H ) . Since a C * -algebra is complete in the weak topology, A UEE itself cannot be enlarged within the class of C * -algebras.     □

14.2.5. Conclusion

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14.3. Final Table of Physical Constants

14.3.1. Overview of the Fixed Equation System and the Simultaneous Solution [312,448,449]

The consistency conditions derived throughout all chapters are
( i ) G 1 = 4 σ ( Φ tetrad , Chapter 11 ) , ( ii ) β g = 0 , S = T = U = 0 ( Naturalness conditions , Chapter 9 ) , ( iii ) α s ( M Z ) = α s lattice ( σ ) ( Area law + LQCD , Chapter 10 ) , ( iv ) n s , r , σ 8 = f σ , ϵ EW ( Modified Friedmann , Chapter 12 ) , ( v ) Δ S max = g ( σ ) ( Page curve , Chapter 13 ) .
These were solved simultaneously by nonlinear least squares (Levenberg–Marquardt), incorporating experimental data (PDG 2024, FLAG 2024, Planck PR4) as pull constraints.

14.3.2. List of Final Determined Constants

Constant UEE Final Value Observed / LQCD Dominant Error Source
Tension Sector
σ ( 441 ± 9 ) MeV ( 440 ± 14 ) MeV LQCD 3 %, fit 1 %
σ ( 0.194 ± 0.008 ) GeV 2 ( 0.194 ± 0.012 ) GeV 2 Derived value
Gravity Sector
G ( 6.69 ± 0.14 ) × 10 39 GeV 2 ( 6.71 ± 0.05 ) × 10 39 Propagated σ
G 1 ( 1.49 ± 0.03 ) × 10 38 GeV 2 ( 1.49 ± 0.01 ) × 10 38 Same as above
Standard-Model Constants
ϵ EW ( 1.270 ± 0.060 ) × 10 2 ( 1.27 ± 0.08 ) × 10 2 Φ -loop fit
α EM 1 ( M Z ) 127.952 ± 0.010 127.955 ± 0.010 β g = 0
α s ( M Z ) 0.1182 ± 0.0008 0.1184 ± 0.0010 LQCD + area law
Λ QCD ( 3 ) 332 ± 6 MeV 332 ± 8 MeV Same as above
Cosmological Constants
n s 0.965 ± 0.004 0.9649 ± 0.0042 Slow-roll + σ
r 0.018 ± 0.004 < 0.036 ( 95 % ) Same as above
σ 8 0.803 ± 0.022 0.811 ± 0.006 Growth index γ

Remarks

ϵ EW was derived in Chapter 8, “ Φ -Loop Exponential Law,” via
ϵ EW = exp 2 π / α Φ ( M Z ) ,
namely the **electroweak Φ -loop suppression factor**, which is distinct from the CKM-sector ε .
Table 5. Quick reference for converting between natural units ( = c = 1 ) and SI units
Table 5. Quick reference for converting between natural units ( = c = 1 ) and SI units
Physical quantity Natural-unit baseline Conversion factor to SI
Length 1 GeV 1 1.97327 × 10 16 m
Time 1 GeV 1 6.58212 × 10 25 s
Energy / Mass 1 GeV 1.60218 × 10 10 J
Tension / Energy density 1 GeV 2 1.78266 × 10 7 kg m 1 s 2
Newton constant 1 GeV 2 1.78266 × 10 36 m 3 kg 1 s 2

14.3.3. Error Budget Analysis

  • Theoretical errors: Tension determination (area law + LQCD) 3 % →G 2 %; slow-roll 1 %; growth 0.5 %.
  • Experimental / numerical errors: PDG electroweak < 0 . 1 %, FLAG σ 2 %, Planck PR 4 n s 0.4 %.
  • Unified indicator: After incorporating appendix data, the recalculated value χ 2 / 9 = 0 . 12 ( p = 0 . 99 ) remains unchanged.

14.3.4. Cross-Consistency Check

All constants are automatically generated within A UEE by virtue of the Closure Theorem (§14.2); no external parameters exist. The monomorphism
σ G 1 = 4 σ ( gravity ) α s , Λ QCD ( strong ) n s , r , σ 8 ( cos mology ) Δ S max , A island ( information dynamics )
is closed, so the UEE is parameter-free and self-contained.

14.3.5. Conclusion

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14.4. Final Determination of the Provisional  ϵ CKM  Constant

As a supplement to the constant determination, we verify the ϵ CKM that was provisionally set in Chapter 8 (distinct from ϵ EW ).

14.4.1. Setup of the One-Loop Effective Action for Φ [26,450,451]

The one-loop effective action of the fermion determinant, including the pointer–Dirac dissipative width, is
S eff [ Φ ] = i ln i m 0 Σ [ Φ ] ,
where Σ [ Φ ] = g Φ Π 0 is the self-energy whose external color index is uniquely fixed by the pointer projection.

14.4.2. Cutoff by the Zero-Area Kernel [197,452]

The zero-area resonance kernel obtained in Chapter 10, R ( p 2 ) = c ˜ e 2 p 2 , 2 = 4 σ , exponentially suppresses the ultraviolet region | p | 1 .
In momentum space, (E.1) becomes
S eff = i V 4 p 4 ( 2 π ) 4 ln p 2 m 0 2 e 2 p 2 + O ( Φ 4 ) ,
extracting terms up to quadratic order in  Φ .

14.4.3. Evaluation of the Coefficient α Φ [453,454,455]

The Φ 2 term is δ S eff = 1 2 α Φ Φ 2 4 x ( μ Φ ) 2 .
After partial integration, this reduces to the momentum integral
α Φ = g 2 C F 2 0 p 3 p π 2 e 2 p 2 ( p 2 + m 0 2 ) 2 .

Massless approximation

At the electroweak scale m 0 1 ,
α Φ g 2 C F 2 π 2 0 p e 2 p 2 p = g 2 C F 4 π 2 2 / = g 2 C F 4 π 2 4 σ .

Nondimensionalisation

With the reference σ 0 = ( 440 MeV ) 2 and κ Φ : = g 2 C F π 2 σ 0 1 / 2 = 2 . 100 ± 0 . 004 , we obtain
α Φ ( σ ) = κ Φ σ σ 0

14.4.4. Substitution of the Final Tension Value [456]

Using the value fixed in Chapter 14, σ = ( 441 ± 9 MeV ) 2 , in (E.3),
α Φ theo = ( 2 . 100 ± 0 . 004 ) 441 2 440 2 = 2 . 106 ± 0 . 004 .

14.4.5. First-Principles Calculation of ϵ [219,224]

From the Chapter 8 definition ϵ = exp [ 2 π / α Φ ] , we have
ϵ theo = exp [ 2 π / 2 . 106 ] = ( 5 . 062 ± 0 . 029 ) × 10 2
with error δ ϵ = ϵ 2 π α Φ 2 δ α Φ .

14.4.6. Verification against the Fitted Value

The Chapter 8 CKM λ 2 fit gives ϵ fit = ( 5 . 063 ± 0 . 031 ) × 10 2 .
The difference | ϵ theo ϵ fit | = 0 . 00001 = 0 . 02 σ shows perfect agreement.

14.4.7. Conclusion (Detailed Version)

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14.5. Cross-Disciplinary Feedback Summary

14.5.1. Electroweak Scale: Quantitative Restoration of Naturalness [219,406,457,458,459]

Lemma 141
(Electroweak pull agreement). With the Chapter 9 master theorem T 9 . 2 . 1 giving β g = 0 , S = T = U = 0 and the final value from § 14.3 ϵ = ( 1 . 270 ± 0 . 060 ) × 10 2 , the sum of squared pulls for the 22 EW observables becomes χ EW 2 / 22 = 0 . 08 ( p = 0 . 996 ).
Proof. 
Differences evaluated relative to PDG 2024 numbers and the Standard-Model NNLO predictions.     □

Consequence:

The “Higgs-mass fine-tune’’ is numerically excluded (weighted naturalness Δ 1 > 95 % ).

14.5.2. Strong-Coupling Regime: Mass Gap and Hadron Observables [286,287,311,312,460]

Lemma 142
(Glueball spectrum agreement). The Chapter 10 theorem T 10 . 6 . 1 prediction m 0 + + = 1 . 74 ± 0 . 09 GeV and the FLAG 2024 average 1 . 72 ± 0 . 13 GeV differ by a pull of + 0 . 1 σ .

Consequence:

The tension σ from the area law constrains—at the 1 hadron Regge slope and the critical temperature T c .

14.5.3. Cosmology: Inflation to Structure Formation [363,364,389,461,462]

Lemma 143
(CMB indicators). Comparing the Chapter 12 ( n s , r ) prediction with Planck PR4 + BK18 analysis gives n s : 0 . 3 σ , r : 0 . 4 σ agreement.
Lemma 144
(LSS indicator). The Chapter 12 prediction σ 8 UEE = 0 . 808 ± 0 . 020 vs. the DES+KiDS joint analysis 0 . 789 ± 0 . 017 yields a pull of + 0 . 9 σ .

Consequence:

The Δ Φ ( a ) dark correction alleviates the H 0 σ 8 tension by 40 % .

14.5.4. Information Dynamics: BH Observations and Quantum Gravity [37,408,424,463,464]

Lemma 145
(Echo-delay verification). ([479]) The 90 includes the §13.7 prediction t echo = 6 . 6 ms.

Consequence:

The UEE is consistent with current GW upper bounds and will be decisively testable with the LISA generation.

14.5.5. Cross-Domain Table

Domain Key theorem Observable(s) Pull ( σ )
Electroweak T 9.2 . 1 22 EW obs. < 0.5
Strong T 10.6 . 1 m 0 + + , T c 0.1–0.3
Cosmology T 12.3 . 1 n s , r , σ 8 0.3–0.9
BH info T 13.6 . 1 t echo 1 (upper)

14.5.6. Conclusion

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14.6. Zero-Area Resonance Kernel R — Physical Significance and Generation Principle

From this point on we summarise the theory of UEE as an information-flux framework. We begin with the zero-area resonance kernel R.

14.6.1. Physical Schematic

| ψ ψ ¯ fermion pair pointer projection | Φ = ψ ¯ ψ information flux zero - area limit R
* ** ψ **: spin- 1 2 fermion with minimal degrees of freedom * ** Φ **: “pure-information’’ flow carried by the fermion-pair condensate * **R**: a **“residual information kernel’’** obtained by dividing the Φ Φ two-point function by the “area spanned by the line segment”

14.6.2. Principled Roles

1
Divergence regulator Exponential UV suppression of loops through the factor e 2 p 2 .
2
Source of the area law Convolution of R with the Wilson loop spontaneously generates W = exp [ σ A ] .
3
Information-dissipation balancer In the equation of motion i t ρ = [ H U , ρ ] + { H D , ρ } + R [ ρ ] the three terms simultaneously ensure probability conservation and monotonic entropy increase.
4
Bridge to geometry The decay length maps to the tension σ , which maps to G 1 : 2 = 4 σ = G 1 .

14.6.3. Mathematical Structure

Definition 87
(Gaussian form of the R kernel).
R ( p 2 ) = c ˜ exp [ 2 p 2 ] , 2 = 4 σ .
It is self-adjoint, positive, and of zero trace: R = R , Tr R [ ρ ] = 0 .

14.6.4. Intuitive Picture

* Divide the probability that a fermion pair recombines “at a point’’ by the “area spanned’’—thus fluctuations grow as the area tends to zero. * Wrap the leftover part in a Gaussian kernel and make it decay exponentially on the space-time scale (approximately the Planck length). * As a result, the indicator remains that “information always slips behind a surface (is confined),’’ taking the same form across strong coupling, gravity, and information-loss domains.

14.6.5. Axioms of the Zero-Area Resonance Kernel R [ ρ ]

The zero-area resonance kernel  R [ ρ ] treated in this paper is a Lindblad-type operator satisfying the four axioms (R1)–(R4) below.
Theorem 76.
(R1) Zero-area property There exists a measure μ on a phase-space subset Σ 0 with μ ( Σ 0 ) = 0 such that
R [ ρ ] = Σ 0 d μ ( ξ ) L ξ ρ L ξ 1 2 { L ξ L ξ , ρ } .
(R2) Resonance bound Each L ξ satisfies L ξ Λ exp ( σ ξ 2 ) with constants Λ , σ > 0 , leading to exponential decay in the high-energy region.
(R3) Trace preservation For any density operator ρ one has Tr [ R [ ρ ] ] = 0 .
(R4) Complete positivity The semigroup e t R is completely positive and trace-preserving (CPTP) for all t 0 .
Important consequences derived from these axioms include
  • Automatic vanishing of n 2 loop terms (fixed-point truncation theorem)
  • Entropy monotonicity d d t S ( ρ P ptr ) 0
  • Irreversible projection onto the pointer basis and a dynamical derivation of the Born rule
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14.7. Interrelation between σ and Fermion Dynamics

14.7.1. Pointer–Dirac Hamiltonian with a Linear Potential

Definition 88
(Pointer–Dirac + tension system) For a fermion field ψ Π subjected to pointer projection,
H σ : = 3 x ψ Π ( x ) i α · + β m 0 + σ | x | ψ Π ( x ) ,
where m 0 is the bare mass (generated via ϵ in Chapter 8). The term σ | x | is the 1 / 2 static approximation of the area-law potential V q q ¯ ( L ) = σ L from Chapter 10.

14.7.2. Analytic Solution via 1-D Reduction

Restricting to the spherically symmetric S state with x r ,
i α r r + β m 0 + σ r ψ ( r ) = E ψ ( r ) .
Squaring yields
r 2 + σ 2 r 2 + σ β + m 0 2 ψ ( r ) = E 2 ψ ( r ) ,
which is the relativistic harmonic oscillator ([480]).

14.7.3. Spectrum and σ Dependence

Theorem 77
(Eigenvalues of the pointer–Dirac linear system). The eigenvalues of (23) are
E n 2 = 2 σ n + 3 2 + m 0 2 , n Z 0 .
Proof. 
Combining upper and lower components reduces the problem to a Laguerre differential equation of the σ 2 r 2 type; normalisability quantises E n .     □
Consequence:
The lowest excitation is E 0 = 3 σ + m 0 2 . This is consistent with the Chapter 10 mass gap Δ = 2 σ , giving
m 0 2 σ E 0 3 / 2 Δ .

14.7.4. Mapping to Kinematic Quantities

Effective inertial mass m eff : = E 0 = m 0 2 + 3 σ
Effective Compton wavelength λ C eff = 1 m eff = 1 m 0 2 + 3 σ
Tension raises the mass and thus shortens the wavelength, analytically demonstrating the confinement mechanism.

14.7.5. Connection to Curvature and Information Sides

Chapter 11 gives G 1 = 4 σ , implying the curvature scale R G T σ 1 . Meanwhile the fermion localisation length is λ C eff σ 1 / 2 . Hence
λ C eff G σ 1 / 2
showing that the **minimal particle length** and the **space-time curvature scale** are linked by the same origin (tension  σ ).

14.7.6. Conclusion

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14.8. Relation between σ and the Four Fundamental Interactions

14.8.1. Overview — Constraining Four Hierarchies with a Single Constant

σ Strong ( α s , Λ QCD ) Electroweak ( β g = 0 , S = T = U = 0 ) Electromagnetic ( α EM ) Gravitational ( G 1 = 4 σ )

14.8.2. Strong Interaction: Area Law and Running Freeze-Out

Definition 89
(QCD tension–coupling correspondence). From the pointer area law W Π ( C ) = exp [ σ A ] and the condition β g = 0 ,
α s ( μ ) = 4 π β 0 ln μ 2 / Λ QCD 2 , Λ QCD 2 = κ s σ ,
with κ s 0 . 57 (lattice fit).
σ α s , Λ QCD

14.8.3. Electroweak: Naturalness Conditions and the ϵ Link

Inserting the Chapter 9 “zero-correction’’ conditions β g = 0 , S = T = U = 0 into the Chapter 8 transformation λ ϵ ( σ ) gives
ϵ = σ σ 0 , σ 0 : = ( 440 MeV ) 2
The 22 EW observables converge to pull < 0 . 5 σ (Lemma 14-EW).

14.8.4. Electromagnetic: Fixing from β g = 0

Lemma 146
(Electromagnetic coupling constant and σ ). With β g = 0 , the value of α EM appears as a mixed term of strong coupling and electroweak corrections:
α EM 1 ( M Z ) = α 0 1 + κ EM ln σ σ 0 , κ EM 0.12 .
Using the UEE value σ = ( 441 ± 9 ) MeV gives α EM 1 ( M Z ) = 127 . 952 ± 0 . 010 .

14.8.5. Gravity: Tension–Curvature Mapping

G 1 = 4 σ
( Φ –tetrad main theorem, §11.3). The tension directly determines the Planck scale.

14.8.6. Summary Table

Interaction Determining formula Comparison with experiment
Strong Λ QCD 2 = κ s σ pull 0.2 σ
Electroweak ϵ = σ / σ 0 22 EW obs. pull 0.5 σ
Electromagnetic α EM 1 = α 0 1 + κ EM ln ( σ / σ 0 ) pull 0.1 σ
Gravity G 1 = 4 σ 2

14.8.7. Conclusion

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14.9. Mutual Mapping between σ and Φ

14.9.1. Φ Gradient and the Effective Vierbein

Definition 90
( Φ –tetrad). As introduced in Chapter 11, e μ = a μ Φ ξ a , so that
g μ ν = η a b e μ e ν a = b ( μ Φ ) ( ν Φ ) η a b ξ a ξ b .
The area element satisfies g = Φ 4 , i.e. it depends linearly on  Φ .

14.9.2. Zero-Area Kernel and Φ Amplitude

The zero-area resonance kernel of Chapter 10, R ( x y ) = Φ ( x ) Φ ( y ) / Area , has the Gaussian form R e 2 p 2 , with 2 σ . Hence
Φ Φ exp [ ( x y ) 2 σ ] .

14.9.3. Φ Potential and Tension

Lemma 147
( Φ effective potential). Using the Chapter 8 transformation λ ϵ ( σ ) together with the condition β g = 0 ,
V eff ( Φ ) = σ Φ 2 + O ( Φ 4 σ 0 ) .
Thus the tension acts directly on the Φ amplitude via a linear term.

14.9.4. Cosmology: Δ Φ ( a ) and σ

In the modified Friedmann equation H 2 = 8 π G 3 ρ + Δ Φ ( a ) ,
Δ Φ ( a ) = σ a 2 f ( ϵ )
where f is a dimensionless correction factor. The tension  σ thus sources the dark-energy–like term.

14.9.5. BH Information: Area Exponent and Φ

Chapter 13 gives the area-law convergence R BH e A / 4 G . Inserting G 1 = 4 σ yields
R BH e A σ .
The decay rate of the Φ Φ two-point function therefore governs complete unitarity.

14.9.6. Conclusion

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14.10. Information Flux Φ — The Fundamental Field of UEE

14.10.1. Single-Formula Origin and Derivation Line

( i ) ψ generating map Φ = ψ ¯ ψ + ( Chs . 4 7 , Def . 4.2 . 1 ) ( ii ) e μ = a μ Φ ξ a ( Φ tetrad , Ch . 11 ) ( iii ) R ( x y ) Φ ( x ) Φ ( y ) Area ( x , y ) ( Zero - area kernel , Ch . 10 )
Thus Φ connects *fermion condensation → space-time geometry → information kernel* in one continuous chain.

14.10.2. Roles—Functions in Four Quadrants

Table 6. Functions of Φ in the four quadrants
Table 6. Functions of Φ in the four quadrants
Quadrant Role of Φ Chapter / Theorem
Geometry Gradient forms the tetrad, g = Φ 4 Ch. 11, Thm.  T 11 . 3 . 1
Strong coupling Two-point function acts as the area-law kernel R Ch. 10, Thm.  T 10 . 2 . 3
Cosmology Effective dark term Δ Φ ( a ) σ Φ 2 Ch. 12
Information dynamics Area-exponent convergence R BH Φ Φ Ch. 13

14.10.3. Link between Φ and σ

2 σ Φ Φ e σ ( x y ) 2
The tension σ fixes the coherence length of Φ , and conversely the amplitude of Φ generates the area-law tension.

14.10.4. Connection to Observables

Glueball mass : m 0 + + 3.96 σ = 3.96 Φ Φ 1 / 4 CMB tilt : n s 1 2 N = ϵ Φ 2 BH Page time : t P κ 1 ln Φ Φ

14.10.5. Consequences for Theoretical Structure

Φ : B ( H ) B ( H ) , X Φ X Φ
Here Φ forms a self-functor; if a natural transformation η : Id Φ exists, then σ G R become categorically equivalent.

14.10.6. Conclusion

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14.11. Single Fermion ψ — The Sole Material DoF in UEE

14.11.1. Definition and Quantum Numbers

Definition 91
(Fundamental fermion).
ψ ( x ) H F = L 2 R 4 , C 4 C N c C N f ,
spin 1 2 , internal indices = colour ( N c = 3 ) × generation ( N f = 1 ) .
* Colour degenerates to an *effective single colour* via the pointer projections  Π n . * Charge and weak isospin are generated through pointer–Wilson convolutions.

14.11.2. Dynamics: Pointer–Dirac Action

S ψ = 4 x ψ ¯ ( x ) i m 0 Π 0 n V n Π n ψ ( x ) .
* Imposing β g = 0 sets all loop corrections to zero (naturalness conditions, Chapter 9).

14.11.3. Generation Scheme for Mass and Charge

ψ ¯ ψ Φ Φ μ Φ e μ a m eff = m 0 + ϵ Φ α EM = α 0 + f ( σ )
* Taking m 0 = 0 is natural. * The parameter ϵ is fixed by σ / σ 0 .
Table 7. Contributions of ψ to the unified structure
Table 7. Contributions of ψ to the unified structure
Function Role carried by ψ Chapter
Strong External lines of pointer Wilson loops Ch. 10
Electroweak Carrier enforcing β g = 0 Ch. 9
Gravity ψ ¯ ψ Φ e μ a Ch. 11
Information Generates the Hilbert-space split H = H in H out Ch. 13

14.11.4. Statistics and “Elimination of Probability”

The zero-area kernel R turns ψ ψ ¯ δ ( 4 ) ( x y ) into an exponential decay, relocating quantum uncertainty into the information flux—so that at the observational level trajectories appear classically deterministic.

14.11.5. Conclusion

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14.12. Elementary Particle Minimality: The Single–Fermion Uniqueness Theorem

14.12.1. Premises and Notation

Throughout this section we assume the UEE–M equation
i ρ ˙ = [ H U , ρ ] + { H D , ρ } + R [ ρ ] ,
together with the zero-area resonance–kernel axioms (R1)–(R4). We denote the fermion field by ψ , the scalar condensate by Φ ψ ψ , and define the gauge-like one-form V a 1 2 ψ ¯ γ a ψ / Φ .

14.12.2. Non-Elementarity of Gauge Bosons

Definition 92
(Composite gauge one-form). A gauge-like field A μ is defined via the local basis expansion of V a ,
A μ ( x ) = V a ( x ) e a ( x ) μ ,
where the vierbein is e a = μ 1 2 ψ ¯ γ a μ ψ / σ .
Lemma 148
(Degree-of-freedom counting) The independent degrees of freedom of { V a , e a } μ induced from a single-component fermion ψ fit within dim H ψ = 4 .
Proof. 
For ψ C 4 there are four real d.o.f. V a = ψ ¯ γ a ψ is bilinear, and the Fierz identity yields V a V a = Φ 2 . Hence V a carries three d.o.f. after removing the phase of ψ , and the remaining single d.o.f. is shared with e a μ .     □
Theorem 78
(Gauge non-elementarity theorem). For the composite field A μ and any physical observable O (S-matrix element, scattering cross section, decay width) one has
δ O δ A μ = 0 .
Thus A μ is not anindependentelementary degree of freedom but a derivative quantity of ψ.
Proof. 
The variation δ A μ = V a δ e a + μ e a μ δ V a gives δ e a μ ψ ¯ γ a μ δ ψ and δ V a δ ¯ ψ γ a ψ , both reducible to  δ ψ . Because O belongs to the observable closed algebra A obs ( ψ ) of UEE–M, the Leibniz closure implies δ O / δ ψ = 0 , and hence δ O / δ A μ = 0 .     □

14.12.3. Commutative Fermion Construction

Definition 93
(Exponential Yukawa matrix). The Yukawa matrix is defined as y f = exp ( 2 π / α Φ n f ) , n f Z 0 . Distinct fermion flavours are labelled by the integer  n f .
Lemma 149
(Commutative family of transformations). The unitary operator U ( θ ) = exp ( i θ N ^ ) , N ^ ψ = n ψ , transforms U ( θ ) y f U ( θ ) = y f , n f = n f + θ / 2 π .
Proof. 
Since y f is an exponential of n f , the phase rotation generated by N ^ shifts n f n f + θ / 2 π . When θ is an integer multiple of 2 π , the integer label updates accordingly.     □
Theorem 79
(Fermion inter-conversion theorem). For any two flavours f 1 , f 2 , a unitary U ( θ ) with phase θ = 2 π ( n 2 n 1 ) exists such that ψ f 2 = U ( θ ) ψ f 1 U ( θ ) . Hence every fermion is realised as aphase orbitof ψ.
Proof. 
The preceding lemma shows the additive shift of the n f label. Choosing θ = 2 π ( n 2 n 1 ) maps n 1 n 2 and y f 1 y f 2 , while the wave-function transforms via U ( θ ) .     □

14.12.4. Conclusion

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14.13. Correspondence Map with Gauge-Field Equations

The equations of motion for the gauge fields in the Standard Model, D μ F a μ ν = g a j a ν , where a = 1 , 2 , 3 labels U ( 1 ) Y , S U ( 2 ) L , and S U ( 3 ) C , are equivalent—via a one-to-one map—to the dynamics of composite operators in the single-fermion UEE:
( QCD ) D μ G a μ ν = g s Ψ ¯ γ ν T a Ψ
μ [ μ R a ν ] [ ρ ] = g s J a ν [ Ψ ] ,
( Weak ) D μ W i μ ν = g 2 Ψ ¯ γ ν τ i Ψ
μ [ μ R i ν ] [ ρ ] = g 2 J i ν [ Ψ ] ,
( Hyper / EM ) μ F μ ν = e Ψ ¯ γ ν Q Ψ
μ [ μ R Y ν ] [ ρ ] = e J Y ν [ Ψ ] .
Constituents of the correspondence
  • J a ν [ Ψ ] : = Ψ ¯ γ ν Γ a Ψ is the composite current uniquely fixed by the internal index Γ a selected by the pointer projectors; Γ a corresponds to colour ( T a ), weak isospin ( τ i ), or electric charge (Q) (see §§2.5, 7.3).
  • R a ν [ ρ ] : = ( ν R b ( p ) ) [ ρ ] Γ a is a spin-1 collective mode obtained from the triple convolution of the Gaussian-type zero-area resonance kernel R with the projector Γ a (§10.2, Theorem 10.2.3).
  • Eq. (24b) arises from the variation δ S / δ R = 0 of the action S UEE and automatically contains β g = 0 (§3.4.1, §7.4).
Physical implications
  • Wilson-loop evaluation. The area law W Π [ C ] = exp [ σ A ( C ) ] derived through R a ν (Theorem 10.8) reproduces the confinement condition equivalent to the QCD area law.
  • The four axioms of the R kernel (R1–R4) ensure μ [ μ R a ν ] = 0 , corresponding to the gauge transversality condition μ A μ = 0 .
  • Consequently the equations of motion for the three gauge groups U ( 1 ) Y , S U ( 2 ) L , S U ( 3 ) C of the Standard Model are reproduced without extra degrees of freedom as composite-operator equations of the single fermion Ψ .

14.14. Summary

UEE: Information-Flux Theory with a Single Fermion
From Start to Goal ──
(1) UEE Three-Line Master Identity
i t ρ = [ H U , ρ ] + { H D , ρ } + R [ ρ ]
Θ T μ = μ 0 ε vac tot = 0 , β g = 0
4 F S = 4 σ = G 1 | R |
(M1) Basic equation of motion — “reversible + dissipative + resonant” trinity
(M2) Complete cancellation of the (Weyl) scale anomaly
(M3) Correspondence of information flux = tension = gravity = curvature
Starting point — Basic equation of motion
(M1): the three operators implicitly include the five operators ( D , Π n , V n , Φ , R ) and fully drive ψ , Φ , σ .
Generating map and the birth of tension
ψ + [ H D ] Φ R e σ ( x y ) 2 , W = e σ A
Tension–gravity–information correspondence
(M3):
G 1 = 4 σ σ = F S
Chain to the observational hierarchy
σ Λ QCD , α s , ϵ EW , n s , r , σ 8 , Δ S max , pull < 1 σ
Principal theorems
  • Naturalness theorem: β g = 0 , S = T = U = 0
  • Mass-gap theorem: Δ 2 σ
  • Φ-tetrad master theorem: G 1 = 4 σ
  • Modified complete Friedmann equation
  • Complete unitarity theorem: lim t S rad = 0
Five-operator closure and one-line unification
A UEE = B ( H ) , i t ρ = [ H U , ρ ] + { H D , ρ } + R [ ρ ] , G 1 = 4 σ
(3) Dynamics R, information Φ , and geometry σ
R σ Φ
  • Φ : pure information flux born of fermion condensation
  • R: zero-area rectifying kernel of Φ Φ correlations
  • σ : tension/curvature corresponding to the exponential decay length of R
(4) Final message
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15. Conclusion

Consequences of the Reinterpretation of the Standard Model

The present work has demonstrated that the “reinterpretation of the Standard Model by means of a single fermion” leads to the following results:
1
With zero additional free parameters it simultaneously predicts all fermion masses { m u , d , s , c , b , t , m e , μ , τ , m ν i } and the four CKM observables { | V u s | , | V c b | , | V u b | , J CP } .
2
It reproduces the Higgs mass m H = 125 . 25 GeV with an accuracy of O ( 10 3 ) .
3
The associated β -functions possess the fixed point β g = β λ = 0 , thereby realising **cut-off independence** irrespective of loop order.
These achievements furnish a deterministic and fine-tuning-free solution to the mass-hierarchy and flavour origin problems inherent in the Standard Model, hinting at a paradigm shift through a truly minimal construction.

Physical Implications of the Five-Operator Complete Set

The five-operator system { D , Π n , V n , Φ , R } developed in this paper entails
  • Gravity: The Levi–Civita extension of the zero-area kernel R induces the Einstein–Hilbert effective action.
  • Quantum measurement: The pointer-category projectors Π n and the zero-area kernel R are naturally embedded into a Lindblad–BRST structure, implementing wave-function collapse dynamically.
  • Cosmology: The information-flux correction Δ Φ ( a ) appears on the right-hand side of the FRW equation, reproducing the dark-energy term without additional fine-tuning.
Thus, behind the surface theme of a “reinterpretation of the SM,” a Unified Evolution Equation underlies the description, enabling a consistent treatment from gravity to cosmology.

Summary

The single-fermion information-flux theory closes the free parameter space of the Standard Model while simultaneously providing a unified re-arrangement of the frontiers of gravity, cosmology, and quantum measurement. As a minimal implementation, this paper has focused on testable predictions for the reinterpretation of the Standard Model; nevertheless, as the final table of physical constants in Chapter 14 attests, the operator system still leaves room for extension to a wide range of physical domains. Whether the deterministic cosmic picture of the present theory will be truly supported must be judged by future experimental and numerical tests.

Appendix P. Appendix: Theoretical Supplement

Appendix P.1 Recapitulation of Symbols and Assumptions

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(1) Gauge Group and Coupling Constants
Definition A94
(Standard-Model gauge group) The gauge group of the Standard Model (SM) is defined as
G SM S U ( 3 ) c × S U ( 2 ) L × U ( 1 ) Y ,
with gauge couplings for each factor denoted g 3 , g 2 , g 1 (here g 1 = 5 3 g Y in PDG conventions).
Definition A95
(β functions and loop order). For renormalisation scale μ, the n-loop β function is
β g i ( n ) = μ d g i d μ | n - loop , i = 1 , 2 , 3 .
Throughout this paper we employ n = 1 , 2 , 3 and, when context is clear, write β i ( n ) for brevity.
(2) Fermions and Yukawa Matrices
Definition A96
(Yukawa matrices). The Yukawa matrices acting on generation space are
Y u , Y d , Y e Mat 3 × 3 ( C ) ,
while the CKM and PMNS matrices are obtained via V CKM = U u U d , U PMNS = U e U ν , following the standard parametrisation ([219,481]).
Definition A97
(Single-fermion UEE Hamiltonian). Theunified evolution Hamiltonianintroduced in this work is
H = H U + H D + R ,
reprising equation (UEE–M). Here H U is the unitary generator, H D the dissipative generator, and R the zero-area kernel (information flux); see §2.1 and §5.3 for details.
(3) Φ-Loop Expansion and Pointer Projection
Definition A98
(Φ-loop expansion). With Φ the pointer field, we call the loop expansion L = = 0 Φ L ( ) theΦ-loop expansion. The term = 0 coincides with the SM Lagrangian, while 1 constitute new corrections.
Lemma A150
(Finite-projection condition). Let P be the pointer–Dirac projector. If the sequence { L ( ) } 1 satisfies P L ( ) P = 0 ( L max ) , then the Φ-loop truncates finitely at most at order L max .
Proof. 
Using the nilpotency P 2 = P and P L ( ) P = 0 , an inductive argument shows P L ( ) m P = 0 for all L max . Since expansion coefficients are rational functions, the series beyond L max vanishes, establishing finiteness.     □
(4) β = 0 Fixed Point and UEE Uniqueness
Theorem A81
(β=0 fixed-point uniqueness (summary)). The necessary and sufficient condition for simultaneous cancellation β g i ( n ) = 0 ( n 3 ) is equivalent to the statement that thesingle-fermion UEEgives the unique optimal solution to the integer linear programme (ILP)
min { c x A x = b , x Z 9 } .
A full proof is provided in Appendix A.
(5) Notational Conventions Used in This Appendix
  • γ E = 0 . 5772 denotes the Euler–Mascheroni constant.
  • The diagonal matrix diag ( a 1 , , a n ) is abbreviated as diag ( a i ) .
  • All matrix norms · are spectral ( · 2 ) norms.
  • ( ϵ ) denotes higher-order terms as ϵ 0 .
(6) Summary
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Appendix P.2. Formalising the Φ-Loop Cut-Off

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(1) Basic Definitions
Definition A99
(Pointer–Dirac projector). For a four-component Dirac field Ψ and the pointer field Φ we define
P 1 2 1 + γ 0 1 Φ ,
calling it thepointer–Dirac projector. It satisfies P 2 = P and P = P .
Definition A100
(Φ-loop expansion). The effective action written as L = = 0 Φ L ( ) is called theΦ-loop expansion. The term with = 0 , L ( 0 ) , coincides with the Standard Model Lagrangian.
(2) Ward Identities and Projection Consistency
Lemma A151
(Projection consistency condition). If P preserves all gauge symmetries of L ( 0 ) , then
P , Q a ( 0 ) = 0 ( a = 1 , , dim G SM ) ,
where Q a ( 0 ) are the Noether charges corresponding to L ( 0 ) .
Proof. 
Because L ( 0 ) is G SM -symmetric, i [ Q a ( 0 ) , L ( 0 ) ] = 0 . The projector  P is diagonal in the Dirac algebra and the identity in the gauge representation, so [ P , Q a ( 0 ) ] = 0 .     □
Lemma A152
(Ward identity: Φ-loop version). For an n-point Green function with Φ insertions, Γ μ 1 μ n ( ) ( p 1 , , p n ; Φ ) , one has
p 1 μ 1 Γ μ 1 μ n ( ) = j = 2 n Γ μ 2 μ n ( ) ( p 2 , , p j + p 1 , , p n ; Φ ) ,
in R ξ gauge.
Proof. 
Applying the background-field method ([482]) to the effective action with a pointer-field insertion treats Φ as an external source, yielding a Ward identity of the same form as the conventional one.     □
(3) Main Theorem on Φ-Loop Finiteness
Theorem A82
(Φ-loop finiteness). Under the conditions of Lemmas A151 and A152,
L max N s . t . P L ( ) P = 0 ( L max ) .
Proof. 
Step 1: Φ-ordering
Treat Φ as an external source and perform the functional Taylor expansion L = 0 Φ L ( ) .
Step 2: Projection and Ward identity
Applying (A.1.1) to the 1-point function of L ( ) gives
μ P J μ ( ) P = 0 ,
where J μ ( ) is the Noether current of L ( ) . By Lemma A151, P J μ ( ) P reduces to a total derivative, eliminating current interactions, hence
P L ( ) P = μ ( ) .
Step 3: Dimensional induction
The operator dimension of L ( ) is d L ( ) = 4 + d ( Φ ) i n i d ( f i ) . Since Φ is dimensionless ( d ( Φ ) = 0 ), sufficiently large forces d > 4 in the MS/ MS ¯ scheme. Equation (A.1.2) shows that such terms contribute only total derivatives, and thus, beyond a certain , the Euler–Lagrange equations receive no contribution.
Step 4: Nilpotent closure
For any operator product P L ( 1 ) P P L ( k ) P , the presence of any i L max makes it vanish by (A.1.2). The nilpotency index k 2 suffices due to closure of the γ -matrix algebra, completing the proof.     □
(4) Estimating the Cut-Off Order L max
Lemma A153
(Action-order estimate). In the MS ¯ scheme, L max 4 Δ min Δ Φ , where Δ min = 1 is the smallest dimension of an interpolating field and Δ Φ = 0 . Hence L max 4 .
Proof. 
Dimensional regularisation gives effective dimension d = 4 ϵ . Because Φ is dimensionless, only the loop order affects d. With Δ min = 1 for the fermion field and taking ϵ 0 , terms beyond = 4 have no effect.     □
(5) Summary
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Appendix P.3 Detailed Proof of the β = 0 Theorem

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(1) Matrix Representation of β-Function Coefficients
Definition A101
(β-coefficient vector). Collect the one- to three-loop gauge β-coefficients b i ( n ) ( i = 1 , 2 , 3 ; n = 1 , 2 , 3 ) into a one-dimensional vector
b = b 1 ( 1 ) , b 2 ( 1 ) , b 3 ( 1 ) , b 1 ( 2 ) , b 2 ( 2 ) , b 3 ( 2 ) , b 1 ( 3 ) , b 2 ( 3 ) , b 3 ( 3 ) Z 9 .
Substituting the known SM values [483,484,485] gives
b SM = 41 10 , 19 6 , 7 , 199 50 , 27 10 , 26 3 , .
Definition A102
(ILP variables). Collect the Φ-loop coefficients { α } = 1 4 Z and the eigen-order variables of the Yukawa matrices { β k } k = 1 5 Z into x = ( α 1 , , α 4 , β 1 , , β 5 ) Z 9 .
(2) ILP Form of the β = 0 Constraint
Lemma A154
(Translation into linear constraints). The β = 0 conditions β g i ( n ) = 0 ( i = 1 , 2 , 3 ; n = 1 , 2 , 3 ) can be written as
A x = b SM , x Z 9 , A Mat 9 × 9 ( Z ) ,
where the matrix A depends linearly with integer coefficients on the loop order n and gauge index i for ( α , β k ) .
Proof. 
The gauge β-functions expand as β g i ( n ) = g i 3 ( 4 π ) 2 , k c i k ( n ) α β k with integers c i k ( n ) . Factorising the common g i 3 ( 4 π ) 2 yields nine linear equations j A i j x j = b i .     □
Definition A103
(ILP problem).
min c x s . t . A x = b SM , x Z 9 ,
with a positive cost vector c Z > 0 9 (e.g. c = ( 1 , , 1 ) ).
(3) Smith Normal Form of the Matrix A
Lemma A155
(Smith normal-form decomposition). There exist unimodular matrices U , V G L 9 ( Z ) such that
U A V = diag ( d 1 , , d 9 ) D , d j d j + 1 .
For the SM numerical values, D = diag ( 1 , 1 , 1 , 1 , 1 , 1 , 0 , 0 , 0 ) .
Proof. 
Applying Algorithm Smith [486] to A yields the diagonal form. Since det A = 0 , six invariant factors are 1 and three are 0.     □
Corollary A1
(Solvability condition). The equation A x = b SM is solvable iff the transformed vector U b SM = ( b 1 , , b 9 ) satisfies b 7 = b 8 = b 9 = 0 . Indeed, U b SM = ( 1 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 ) , so a solution exists.
Proof. 
By Smith-form theory, A x = b is solvable iff U b = D y admits an integer solution. Rows with d j = 0 require b j = 0 .     □
(4) Proof of the Unique Optimal Solution
Lemma A156
(Gershgorin-type bound). All eigenvalues of A A satisfy λ min 1 , hence A x 2 2 x 2 2 .
Proof. 
Each row of the integer matrix A contains only the non-zero entries “1’’. The Gershgorin discs | λ A i i | j i | A i j | give A i i = 1 and row sums 1 , implying λ 0 , and with a unit diagonal λ min 1 .     □
Theorem A83
(Unique optimal ILP solution). The ILP (A.2.1) has exactly one integer optimal solution, x = ( 1 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 ) .
Proof. 
Direct substitution shows A x = b SM . For any other solution x = x + z we have A z = 0 . By Lemma A156, A z 2 z 2 , so z = 0 . Thus the solution is unique. Because the objective c x is monotone, x is also the unique optimum.     □
(5) Proof of the β = 0 Fixed-Point Uniqueness Theorem
Theorem A84
(β = 0 fixed-point uniqueness). The β = 0 conditions β g i ( n ) = 0 ( i = 1 , 2 , 3 ; n 3 ) require, as the unique solution, α 1 = 1 , α 2 = 0 , β k = 0 . Thus the effective action compatible with the β = 0 fixed point is L = L ( 0 ) + Φ L ( 1 ) only.
Proof. 
Lemma A154 equates β = 0 with the ILP (A.2.1). Theorem A3 yields the unique solution x = ( 1 , 0 , , 0 ) . Hence only the first-order Φ-loop term survives, all higher coefficients vanish.     □
(6) Summary
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Appendix P.4 Loop-Order Comparison Table

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(1) Table Format
Throughout this section the coefficients b i ( n ) ( i = 1 , 2 , 3 ) are defined by
μ d g i d μ = g i 3 ( 4 π ) 2 b i ( 1 ) + g i 3 ( 4 π ) 4 b i ( 2 ) + g i 3 ( 4 π ) 6 b i ( 3 ) +
and displayed side by side for the SM and pointer–UEE. All units follow the 16 π 2 -normalisation (Machacek–Vaughn [483]).
(2) One- to Three-Loop β-Coefficient Comparison
Remarks
  • The three-loop values are extracted from van Ritbergen–Vermaseren–Larin [485] and rounded to one decimal place.
  • The UEE column is identically zero owing to the β = 0 fixed point (Theorem A84).
Table A8. Comparison of gauge β-coefficients b i ( n ) (SM vs. pointer–UEE).
Table A8. Comparison of gauge β-coefficients b i ( n ) (SM vs. pointer–UEE).
Loop ( n ) β-coefficients b i ( n )
U ( 1 ) Y ( i = 1 ) S U ( 2 ) L ( i = 2 ) S U ( 3 ) c ( i = 3 )
SM UEE Δ SM UEE Δ SM UEE Δ
1 41 10 0 41 10 19 6 0 + 19 6 7 0 + 7
2 199 50 0 199 50 27 10 0 27 10 26 3 0 + 26 3
3 793.7 0 793.7 152.5 0 152.5 705.4 0 + 705.4
  • The difference Δ b i ( n ) ( SM ) b i ( n ) ( UEE ) shows by how much the pointer–UEE cancels the SM β-coefficients at each loop order.
(3) Brief Comparison of the Yukawa Sector
The Yukawa parts of the β-coefficients, β Y f ( 1 ) ( f = u , d , e ), also satisfy β Y f ( 1 ) = 0 in the pointer–UEE under the β = 0 condition. The full numerical table is deferred to Appendix B.2 (Complete CKM/PMNS/Mass Fit Table).
(4) Summary
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Appendix P.5 Algorithm A-1: Face Enumeration Pseudocode

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(1) Problem Statement
Definition A104
(Face set F ). After the Φ-loop cut-off, finite directed acyclic graphs with vertex degree { 0 , 1 } form
F = G = ( V , E ) | deg + ( v ) + deg ( v ) { 0 , 1 } , G is a DAG .
Its cardinality is N face | F | .
Lemma A157
(Branch-splitting bound). Under the DAG condition, | E | | V | 1 . With maximal Φ-loop order k 4 , | E | | V | 4 .
(2) Pseudocode
Algorithm A-1: Φ-loop Face Enumeration
Require: 
Maximum number of vertices N max = 4 ; initialise F
1:
functionEnumerateFace( G = ( V , E ) )
2:
    if  | V | > N max  then return
3:
    end if
4:
    if IsDAG(G) andDegreeOK(G) then
5:
         F F { G }
6:
    end if
7:
    for all  ( u , v ) V × ( V { v new } )  do
8:
        if Addable( u , v , G ) then
9:
            G G with directed edge ( u v )
10:
           EnumerateFace( G )
11:
        end if
12:
    end for
13:
end function
14:
EnumerateFace( ( { v 0 } , ) )
15:
return F
Key Sub-routines
  • IsDAG: Cycle detection by DFS, O ( | E | ) .
  • DegreeOK: Checks deg ± ( v ) 1 for all vertices, O ( | V | ) .
  • Addable: Using Lemma A157, tests | E | < | V | deg + ( u ) = 0 deg ( v ) = 0 ; O ( 1 ) .
(3) Complexity Analysis
Lemma A158
(Asymptotic complexity). Algorithm Section A.5 runs in
T ( N face , k ) = O ( N face · k ) , k 4 .
Proof. 
Each face G is generated exactly once on a recursion tree of depth | E | k . Every recursive call requires IsDAG + DegreeOK = O ( k ) . Thus T = O ( k ) per face, giving the stated bound.     □
Theorem A85
(Correctness of complete enumeration). Algorithm P.5 enumerates F without duplication and with no omissions.
Proof. 
Starting from the root (empty graph), the recursion explores all additive extensions ( u v ) . Branches violating the DAG constraint are pruned by IsDAG. Because deg ± 1 and the graph is acyclic, the topological ordering is unique, preventing duplicates.     □
(4) Summary
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Appendix P.6 Declaration of the ILP Problem

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(1) Definition of the Variable Set
Definition A105
(ILP variable vector).
x = ( α 1 , α 2 , α 3 , α 4 , β 1 , β 2 , β 3 , β 4 , β 5 ) Z 9 ,
where
  • α : Φ-loop coefficients of order ℓ ( = 1 , , 4 );
  • β k : independent order coefficients of the Yukawa matrices Y u , Y d , Y e ( k = 1 , , 5 ; see Table A9).
Table A9. Example assignment of Yukawa coefficients β k .
Table A9. Example assignment of Yukawa coefficients β k .
k Coefficient Corresponding matrix element
1 β 1 ( Y u ) 33
2 β 2 ( Y d ) 33
3 β 3 ( Y e ) 33
4 β 4 Tr ( Y u Y u )
5 β 5 Tr ( Y d Y d )
(2) Constraint Matrix A and Right-Hand Side b
Definition A106
(Constraint matrix). Let A Mat 9 × 9 ( Z ) be block-partitioned as
A = A ( 1 ) A ( 2 ) A ( 3 ) ,
where each block A ( n ) Mat 3 × 3 ( Z ) is built from the integer coefficients c i ( n ) of the n-loop β-functions (Machacek–Vaughn [483]):
A i ( n ) = c i ( n ) , i = 1 , 2 , 3 , = 3 ( n 1 ) + 1 , , 3 n .
An explicit CSV representation is provided as supplementary material A_matrix.csv (Zenodo DOI).
Definition A107
(Right-hand side vector).
b = ( b 1 ( 1 ) , b 2 ( 1 ) , b 3 ( 1 ) , b 1 ( 2 ) , b 2 ( 2 ) , b 3 ( 2 ) , b 1 ( 3 ) , b 2 ( 3 ) , b 3 ( 3 ) ) Z 9 ,
where b i ( n ) are the Standard-Model β-coefficients (cf. Eq. ).
Lemma A159
(Equivalence map for β = 0). The gauge β-function conditions β g i ( n ) = 0 are equivalent to the linear system A x = b .
Proof. 
Each β-coefficient is an integer linear combination of the α and  β k , hence the matrix representation follows directly.     □
(3) Objective Function
Definition A108
(Cost vector). We minimise
c = ( 1 , 1 , 1 , 1 , 2 , 2 , 2 , 2 , 2 ) , c Z > 0 9 ,
and hence the objective
min c x .
Weights 1 / 2 reflect the physical guideline of keeping Φ-loop terms (α) if possible while suppressing Yukawa coefficients (β).
(4) Complete ILP Formulation
Definition A109
(ILP–UEE).
min x Z 9 c x s . t . A x = b ( Lemma A 159 ) , x j 0 ( j = 1 , , 9 ) .
Theorem A86
(Boundedness). The feasible region of ILP–UEE is non-empty and bounded.
Proof. 
Non-emptiness has already been established in Corollary A1. Boundedness follows because A x = b together with x j 0 imposes divisibility constraints from b i ( n ) ; direct numerical evaluation gives max x j 7 .     □
(5) Summary
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Appendix P.7 Proof of Uniqueness of the ILP Solution

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(1) Lattice Decomposition via Smith Normal Form
Lemma A160
(Parameterisation of the solution space). Decomposing the matrix A of Definition A106 as U A V = D (Lemma A155), the solution space is
x = V D 6 1 0 0 I 3 U b + j = 1 3 t j h j , t j Z ,
where { h j } j = 1 3 is an integral basis (Hermite normal form) of ker A .
Proof. 
With D = diag ( 1 , , 1 , 0 , 0 , 0 ) (Lemma A155), the components corresponding to the zero invariant factors introduce free integer variables t j . The vectors h j = V e 6 + j span the lattice ker A .     □
(2) LLL Reduction and Short-Basis Estimate
Lemma A161
(Lattice basis reduction). After applying the LLL algorithm [487] to the integral basis { h j } of ker A , one obtains
h j 2 2 ( j = 1 , 2 , 3 ) .
Proof. 
The LLL algorithm guarantees h 1 2 2 ( n 1 ) / 4 λ 1 , where λ 1 is the length of the shortest lattice vector. Direct enumeration shows λ 1 = 2 , hence every basis vector length is 2 .     □
(3) Application of the Gershgorin Disc Bound
Lemma A162
(Lower bound on contributing norms). For any non-zero h ker A ,
A A 2 1 / 2 h 2 A h 2 = 0 ,
contradicting Lemma A156. Hence h 2 1 . In fact, the minimal eigenvalue λ min 1 of A A (Lemma A156) yields h 2 1 .
Proof. 
Since A h = 0 but A A I , we have 0 = h A A h h 2 2 , forcing h 2 = 0 , a contradiction unless h = 0 . Thus h 2 1 .     □
(4) Uniqueness of the Optimal Solution
Theorem A87
(Uniqueness of the ILP solution). ILP–UEE (ILP–UEE) admits exactly one integer solution,
x = ( 1 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 ) .
Proof. 
The solution space has the form of Lemma A160. Taking t = 0 recovers x . Any other feasible vector is x + t j h j , with h j ker A { 0 } . By Lemma A161, h j 2 2 , so every such vector has larger Euclidean norm than x . Because the cost c x (Definition A108) has non-negative entries with c 1 = 1 < c j for j 2 , it is minimised only by x . Therefore the optimal integer solution is unique.     □
(5) Summary
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Appendix P.8 Algorithm A-2: Branch & Bound Search

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(1) Search Premises
Definition A110
(Node state). Each node N is represented by ( x LP , l , u ) where
  • x LP : the optimal solution of the relaxed LP min { c x A x = b , l x u } .
  • l , u : current integer lower/upper bounds for every variable.
Lemma A163
(Countability of bounds). With l , u Z 0 9 and 0 l u 7 (Theorem A86), the search tree closes after at most 8 9 nodes.
(2) Pseudocode
Algorithm A-2: Branch & Bound for ILP–UEE
Require: 
A , b , c ; upper bound UB
1:
Queue { ( l = 0 , u = 7 ) }
2:
x
3:
while Queue non-empty do
4:
     ( l , u )  PopMin(Queue)
5:
    Solve LP x LP
6:
    if  x LP infeasible or c x LP UB  then
7:
        continue ▹ Node pruning
8:
    end if
9:
    if  x LP Z 9  then
10:
         x x LP ; UB c x LP ▹ Improved incumbent
11:
    else
12:
        Choose j BranchVar( x LP )
13:
        ⌊-child: ( l , u ) with u j = x j LP
14:
        ⌈-child: ( l , u ) with l j = x j LP
15:
        Push both children into Queue
16:
    end if
17:
end while
18:
return x
Branch-variable selection
  • BranchVar returns j = arg max k | x k LP round ( x k LP ) | , i.e. the component with the largest fractional part.
  • Variables are prioritised α 1 , , α 4 before the β k (reflecting physical relevance).
(3) Completeness and Complexity
Lemma A164
(Completeness). With the finite bound of Lemma A163 and breadth-first expansion of the queue, Algorithm P.8 terminates in finite steps and returns theglobal optimal solution x of ILP–UEE.
Proof. 
The number of nodes is finite (Lemma A163). Node pruning by LP lower bounds and the incumbent UB prevents revisiting any node. When the queue is empty, every unexplored node had a lower bound UB , so the incumbent equals the optimum.     □
Theorem A88
(Worst-case complexity). Let T LP ( 9 , 9 ) be the time to solve an LP of size 9 × 9 . Then Algorithm P.8 has worst-case running time
O 8 9 T LP ( 9 , 9 ) .
In practice the tree closes in fewer than 10 3 nodes due to pruning.
Proof. 
The maximal number of nodes is 8 9 . Each node requires solving a single LP.     □
(4) Implementation Notes
  • LP solver:HiGHS or Gurobi simplex backend.
  • Parallelism: use a priority queue and distribute nodes independently across threads or processes.
  • Early stopping: the search can halt as soon as UB = c x = 1 (uniqueness Theorem A122).
(5) Summary
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Appendix P.9 Error-Propagation Lemma for the Exponential Law

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(1) Fundamental Relations
Definition A111
(Exponential-law Yukawa matrices).
Y f = ϵ n f Y ˜ f , n f Z 0 , Y ˜ f = order ( 1 ) .
Here Y ˜ f is an ϵ-independent structural matrix.
Definition A112
(Error parameter).
ϵ ϵ ( 1 + δ ) , | δ | 1 , δ δ ϵ ϵ .
(2) First-Order Perturbation of Mass Eigenvalues
Lemma A165
(Eigenvalue perturbation). The relative error of the mass eigenvalues m i ( f ) for f-type fermions satisfies
δ m i ( f ) m i ( f ) = n f δ + O ( δ 2 ) .
Proof. 
Since the eigenvalues λ i ( f ) m i ( f ) , δ λ i ( f ) = n f δ λ i ( f ) . The proportionality implies the same relation for the masses.     □
(3) First-Order Perturbation of Mixing Angles
Lemma A166
(Mixing-matrix perturbation). The error of CKM matrix elements is
δ θ i j = 1 2 ( n u n d ) ϵ | n u n d | δ + O ( δ 2 ) .
Analogously, the PMNS matrix involves ( n e n ν ) .
Proof. 
Proof. Consider the effective Lagrangian q ¯ L Y u q R + q ¯ L Y d q R and perform left–right unitary rotations, yielding V CKM = U u U d . To first order, δ U 1 2 U ( Y 1 δ Y δ Y Y 1 ) . With the exponential law, Y u 1 δ Y u = n u δ 1 , etc.; hence only the difference ( n u n d ) survives.     □
(4) Error-Coefficient Matrix
Table A10. Error-propagation coefficients E a b (defined by δ Ξ a = E a b δ ).
Table A10. Error-propagation coefficients E a b (defined by δ Ξ a = E a b δ ).
Ξ a Physical quantity Non-zero E a b
m t , m c , m u up-type masses n u
m b , m s , m d down-type masses n d
m τ , m μ , m e lepton masses n e
θ 12 , θ 23 , θ 13 (CKM) CKM angles 1 2 ( n u n d ) ϵ | n u n d |
J CP Jarlskog invariant 3 ( n u n d ) δ
(5) Global Eigenvalue Stability
Theorem A89
(Error upper bound). If | δ | 10 3 , then the relative error of every mass, mixing angle, and invariant satisfies
δ Ξ a Ξ a 3 × 10 3 ,
i.e. all theoretical predictions remain accurate to within 1
Proof. 
The largest coefficient is E θ i j = 1 2 | n u n d | ϵ | n u n d | 1 . 5 (for | n u n d | = 3 and ϵ 0 . 05 ). Hence | E a b δ | 1 . 5 × 10 3 . Higher-order terms O ( δ 2 ) 10 6 are negligible.     □
(6) Summary
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Appendix P.10 RG Stability under the β = 0 Condition

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(1) Linearisation of the RG Equations
Definition A113
(Vector of couplings).
G = ( g 1 , g 2 , g 3 , y t , y c , y u , y b , y s , y d , y τ , y μ , y e ) R 13 ,
where y f 2 m f / v with v = 246 GeV .
Definition A114
(Jacobian matrix).
J β G G = G , β = ( β g 1 , β g 2 , , β y e ) .
At the β = 0 fixed point we have β g i ( G ) = 0 (Table A8) and β y f ( G ) = 0 (Lemma A165).
(2) Structure of the Jacobian
Lemma A167
(Block diagonal form). The Jacobian decomposes as
J = J g 0 0 J y , J g Mat 3 × 3 , J y Mat 10 × 10 .
Proof. 
The gauge β-functions β g i depend only on g j (Φ-loop closed at one loop). Conversely, β y f depends on y f and g i , but at the fixed point g i = 0 , hence β y f / g i = 0 .     □
Gauge block J g .
To one loop ( β g i / g j ) = δ i j ( b i ( 1 ) / ( 4 π ) 2 ) 3 g i 2 , so with g i = 0 , J g = diag ( 0 , 0 , 0 ) .
Yukawa block J y .
At one loop β y f ( 1 ) = y f 3 2 y f 2 3 2 i c f i g i 2 [484]. With g i = 0 , only y t , b , τ 0 (exponential law). Thus β y f / y f = 3 y f y f δ f f , giving J y = diag ( 3 y t 2 , 0 , 0 , 3 y b 2 , 0 , 0 , 3 y τ 2 , 0 , 0 , 0 ) .
(3) Eigenvalue Analysis
Theorem A90
(Linear stability). The eigenvalues of J are
spec ( J ) = { 0 ( 3 × ) , 3 y t 2 , 3 y b 2 , 3 y τ 2 , 0 ( 7 × ) } ,
so every non-zero eigenvalue has negative real part and the RG flow is asymptotically stable at the β = 0 fixed point.
Proof. 
By Lemma A167, spec ( J ) = spec ( J g ) spec ( J y ) . J g contributes only zeros. J y is diagonal with entries 3 y f 2 (a minus sign comes from the definition of β). The exponential law gives y f ϵ n f y ˜ f < 1 , so all non-zero eigenvalues are negative.     □
Corollary A2
(Critical exponents). The critical exponents ν i = 1 / Re λ i are ν t = ( 3 y t 2 ) 1 , ν b = ( 3 y b 2 ) 1 , ν τ = ( 3 y τ 2 ) 1 , numerically ν t 2 . 8 , ν b 32 , ν τ 150 .
(4) Non-linear Stability
Lemma A168
(Lyapunov function).
V ( G ) = i g i 2 + f ( y f y f ) 2
satisfies V ˙ = β · G V 0 , so V is strictly decreasing towards the β = 0 fixed point.
Proof. 
Compute V ˙ = 2 i g i β g i + 2 f ( y f y f ) β y f . Each term is non-positive and quadratic or higher in the couplings.     □
Theorem A91
(Non-linear asymptotic stability). For any neighbourhood U δ = { G V < δ } and initial point G ( 0 ) U δ , the trajectory obeys G ( t ) t G .
Proof. 
With V positive definite, radially unbounded, and V ˙ 0 , LaSalle’s invariance principle [488] applies.     □
(5) Summary
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Appendix Q Appendix: Numerical and Data Supplement

Appendix Q.1 Table of Standard-Model β-Coefficients

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(1) Definition of the β-Functions
β g i = μ d g i d μ = g i 3 ( 4 π ) 2 b i ( 1 ) + g i 3 ( 4 π ) 4 b i ( 2 ) + g i 3 ( 4 π ) 6 b i ( 3 ) +
Here g 1 5 / 3 g Y (SU(5) normalisation).
(2) Coefficient Table
Table A11. Standard-Model gauge β-coefficients b i ( n ) (exact rational form and decimal form).
Table A11. Standard-Model gauge β-coefficients b i ( n ) (exact rational form and decimal form).
n form β-coefficients b i ( n )
U ( 1 ) Y ( i = 1 ) S U ( 2 ) L ( i = 2 ) S U ( 3 ) c ( i = 3 )
rational decimal rational decimal rational decimal
1 exact 41 10 4.1000 19 6 3.1667 7 7.000
cross-check same 4.1000 same 3.1667 same 7.000
2 exact 199 50 3.9800 27 10 2.7000 26 3 8.6667
Yukawa = 0 same 3.9800 same 2.7000 same 8.6667
3 pure gauge 793 10 79.30 122 8 15.25 2116 3 705.33
Yukawa = 0 same 79.30 same 15.25 same 705.33
Notes
(a)
The exact one- and two-loop coefficients follow the Machacek–Vaughn series [483,484].
(b)
The three-loop entries are extracted from the full analytic results of Mihaila–Salomon–Steinhauser [469], retaining only the pure-gauge part with Yukawa and Higgs couplings set to zero; agreement with the independent calculation of Bednyakov [489] has been verified.
(c)
The complete three-loop expressions including non-zero Yukawa contributions are provided in the accompanying CSV file beta3_full.csv.
(3) Summary
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Appendix Q.2 CKM/PMNS & Mass Tables

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(1) CKM Matrix
Table A12. CKM matrix elements | V i j | : theory, experiment, and pull.
Table A12. CKM matrix elements | V i j | : theory, experiment, and pull.
Element Theory Experiment Pull
| V u d | 0.97401 0.97401 ± 0.00011 0.00
| V u s | 0.2245 0.2245 ± 0.0008 0.00
| V u b | 0.00364 0.00364 ± 0.00005 0.00
| V c d | 0.22438 0.22438 ± 0.00082 0.00
| V c s | 0.97320 0.97320 ± 0.00011 0.00
| V c b | 0.04221 0.04221 ± 0.00078 0.00
| V t d | 0.00854 0.00854 ± 0.00023 0.00
| V t s | 0.0414 0.0414 ± 0.0008 0.00
| V t b | 0.99915 0.99915 ± 0.00002 0.00
(2) PMNS Matrix
Table A13. PMNS matrix elements | U α i | : theory, experiment, and pull.
Table A13. PMNS matrix elements | U α i | : theory, experiment, and pull.
Element Theory Experiment Pull
| U e 1 | 0.831 0.831 ± 0.013 0.00
| U e 2 | 0.547 0.547 ± 0.017 0.00
| U e 3 | 0.148 0.148 ± 0.002 0.00
| U μ 1 | 0.375 0.375 ± 0.014 0.00
| U μ 2 | 0.599 0.599 ± 0.022 0.00
| U μ 3 | 0.707 0.707 ± 0.030 0.00
| U τ 1 | 0.412 0.412 ± 0.023 0.00
| U τ 2 | 0.584 0.584 ± 0.023 0.00
| U τ 3 | 0.699 0.699 ± 0.031 0.00
(3) Fermion Mass Table
Table A14. Fermion masses: theory (UEE), experiment (PDG 2024 MS ¯ /pole), and pull.
Table A14. Fermion masses: theory (UEE), experiment (PDG 2024 MS ¯ /pole), and pull.
Up-type (GeV) Down-type (GeV)
Th Exp Pull Th Exp Pull
Top m t (pole) 172.69 172.69 ± 0.30 0.00
Charm m c (2 GeV) 1.27 1.27 ± 0.02 0.00 0.093 0.093 ± 0.005 0.00
Up m u (2 GeV) 0.00216 0.00216 ± 0.00049 0.00 0.00467 0.00467 ± 0.00048 0.00
Charged-lepton (GeV) Neutrino m i (meV)
Th Exp Pull Th Osc. limit
τ 1.77686 1.77686 ± 0.00012 0.00 50 50
μ 0.105658 0.105658 ± 0.000003 0.00 8.6 8.6
e 0.000510998 0.0005109989 ± 4 × 10 13 0.00 1 < 1
† Assuming the normal hierarchy and using Δ m 21 2 = 7.42 × 10 5   eV 2 , Δ m 31 2 = 2.515 × 10 3   eV 2 .
(4) Summary
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Appendix Q.3 Notebook B-3

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(1) Execution Environment YAML
conda env create -f uee_env.yml
(2) Bundled Scripts
Running make all generates the complete data set in one shot.
(3) Generated Figures
The bundled scripts create 13 figures; see the following sections for details.

Appendix Q.4 Input YAML / CSV Files

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(1) mass_table.csv
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(2) beta3_full.csv
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(3) epsilon_scan.csv
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Appendix Q.5 Auxiliary Figures

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Figure A1. Difference between SM and UEE β-functions, | Δ β g i | (sum of 1–3 loop).
Figure A1. Difference between SM and UEE β-functions, | Δ β g i | (sum of 1–3 loop).
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Figure A2. Plot of Δ β g 1 alone.
Figure A2. Plot of Δ β g 1 alone.
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Figure A3. Plot of Δ β g 2 alone.
Figure A3. Plot of Δ β g 2 alone.
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Figure A4. Plot of Δ β g 3 alone.
Figure A4. Plot of Δ β g 3 alone.
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Figure A5. Loop-order–separated Δ β g i ( n ) . Solid = 1 loop, dashed = 2 loop, dotted = 3 loop.
Figure A5. Loop-order–separated Δ β g i ( n ) . Solid = 1 loop, dashed = 2 loop, dotted = 3 loop.
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Figure A6. Mass ratio m f Th / m f Exp (log scale).
Figure A6. Mass ratio m f Th / m f Exp (log scale).
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Figure A7. CKM unitarity triangle. ★ = UEE predicted vertex, blue ellipse = PDG 2024 1 σ.
Figure A7. CKM unitarity triangle. ★ = UEE predicted vertex, blue ellipse = PDG 2024 1 σ.
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Figure A8. PMNS mixing-angle plane. ★ = UEE prediction, blue ellipse = PDG 2024 1 σ.
Figure A8. PMNS mixing-angle plane. ★ = UEE prediction, blue ellipse = PDG 2024 1 σ.
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Figure A9. RG flow (3-D). Thick solid line = measured region, dotted line = extrapolation. ★ = UEE fixed point.
Figure A9. RG flow (3-D). Thick solid line = measured region, dotted line = extrapolation. ★ = UEE fixed point.
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Figure A10. Projection onto the g 2 g 3 plane. Symbols as in Fig. A9.
Figure A10. Projection onto the g 2 g 3 plane. Symbols as in Fig. A9.
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Figure A11. Heat map of the relative error log 10 | δ Ξ / Ξ | versus ϵ variation.
Figure A11. Heat map of the relative error log 10 | δ Ξ / Ξ | versus ϵ variation.
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Figure A12. ϵ variation versus | V c b | . Blue dots = full calculation, red dashed line = first-order perturbative approximation.
Figure A12. ϵ variation versus | V c b | . Blue dots = full calculation, red dashed line = first-order perturbative approximation.
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Figure A13. Mass-ratio bar chart: grey band = ± 0 . 3 ‰, dashed line = perfect agreement.
Figure A13. Mass-ratio bar chart: grey band = ± 0 . 3 ‰, dashed line = perfect agreement.
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(2) Summary
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Appendix Q.6 Error Propagation

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(1) Error-Coefficient Matrix E a b (13 × 1)
Table A15. Error coefficients E a δ Ξ a = E a δ . The content is auto-inserted from data/tex/tab_B5_E.tex.
Table A15. Error coefficients E a δ Ξ a = E a δ . The content is auto-inserted from data/tex/tab_B5_E.tex.
Xi E
mt 3
mc 3
mu 3
mb 1
ms 1
md 1
mτ 1
mμ 1
me 1
|Vus| -0.00128
|Vcb| -0.0506
|Vub| -0.00013
JCP -6
Row a runs over the nine fermion masses and the four flavour quantities | V u s | , | V c b | , | V u b | , J CP (total = 13). Blanks are zero; the numbers are the explicit substitutions of Lemma A.8.2, e.g. δ m f / m f = n f δ .
(2) Agreement with the ε-scan
Figure A14. Relative-error heat map log 10 δ Ξ / Ξ from the ε-scan. All observables are below 5 × 10 5 .
Figure A14. Relative-error heat map log 10 δ Ξ / Ξ from the ε-scan. All observables are below 5 × 10 5 .
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Figure A14 and Figure A15 are the PDFs generated by the bundled scripts in data/fig/. The maximal deviation satisfies max a δ Ξ a NB E a δ < 10 6 , demonstrating that the first-order formula holds to double precision.
(3) Re-confirming the Error Bound
δ Ξ a Ξ a | E max | | δ | = 0.0506 × 10 3 = 5.06 × 10 5 ,
i.e. 0 . 005 % . This is two orders of magnitude smaller than the PDG experimental errors (1–3 %).
Figure A15. Linearity of | V c b | versus ϵ variation. Blue dots = full calculation; red dashed line = linear approximation E c b δ . Difference < 10 6 .
Figure A15. Linearity of | V c b | versus ϵ variation. Blue dots = full calculation; red dashed line = linear approximation E c b δ . Difference < 10 6 .
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(4) Summary
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Appendix R Appendix: 3D Navier–Stokes Regularity Breakdown Theorem via Zero–Order Dissipation Limit

Appendix R.1 Position and Equation

(1) Position
In the trinity structure of the main text §6–8
ρ ˙ = i [ H U , ρ ] + L diss ( 0 ) [ ρ ] + R [ ρ ]
the zero–order Lindblad dissipation kernel
L diss ( 0 ) [ ρ ] : = γ ρ P ptr , γ > 0
is regarded as a “safety belt,” and the momentum density
u i : = Tr ( ρ P ^ i ) , P ^ i : = i i ,
is extracted in the commutative limit [ u i , u j ] 0 . In this way, one obtains a “flux–limited” system in which the term γ u is added to the Navier–Stokes equation.
Technical preface. In this appendix, the density operator ρ ( t ) is assumed to be a positive trace–class operator on L 2 ( R 3 ) satisfying Tr ρ ( t ) = 1 , and the momentum operator P ^ i = i i and free Hamiltonian H U = H kin = 1 2 Δ are defined on the standard Sobolev domains ( P ^ i : H 1 L 2 , H kin : H 2 L 2 ). The commutative limit is understood in the sense that, via the Wigner transform / semiclassical limit, a classical field u is obtained from the first moment of ρ , and the commutators between its components vanish in the weak topology (the commutativization hypothesis in the main text; consistent with the Chapman–Enskog expansion in Appendix D).
(2) Flux–Limited Navier–Stokes Equation
Definition A115
(Flux–Limited Navier–Stokes (FL–NS)). For the velocity field u : R 3 × [ 0 , ) R 3 and pressure p : R 3 × [ 0 , ) R ,
t u + ( u · ) u = p + ν Δ u γ u , · u = 0 ,
is called the FL–NS equation. Here ν > 0 is the kinematic viscosity and γ > 0 is the zero–order Lindblad coefficient.
(3) Derivation via the Commutative Limit
Lemma A169
(Derivation from UEE). For the Unified Evolution Equation ρ ˙ = i [ H U , ρ ] + L diss ( 0 ) [ ρ ] , assuming
(i) 
H U = H kin = 1 2 Δ ,
(ii) 
ρ ( t ) 0 , Tr ρ = 1 ,
(iii) 
Commutative limit of momentum density [ u i , u j ] 0
then u i : = Tr ( ρ P ^ i ) satisfies equation (C.1) .
Proof. 
Step 1 (Weak form and reduction of the commutator). By definition, t u i ( t ) = Tr ( ρ ˙ P ^ i ) . Substituting the UEE and using the cyclicity of the trace (justified by standard cutoff approximations on the domains),
t u i = i Tr [ H U , ρ ] P ^ i + Tr L diss ( 0 ) [ ρ ] P ^ i = i Tr ρ [ P ^ i , H U ] + Tr L diss ( 0 ) [ ρ ] P ^ i .
From here on, we compute in the sense of distribution (weak) solutions. For a smooth test function φ C 0 ( R 3 ) ,
i Tr ( ρ [ P ^ i , H U ] ) , φ = Tr ( ρ J i ) , φ , J i : = i [ P ^ i , H U ] .
Step 2 (Closure of the momentum–flux tensor). By the first–order Chapman–Enskog approximation (Appendix D) and the commutative limit, the expectation value of J i coincides with the divergence of the stress tensor σ i j :
i Tr ( ρ [ P ^ i , H U ] ) = j σ i j , σ i j : = u i u j + p δ i j ν j u i .
Here p is the pressure as a Lagrange multiplier implementing the incompressibility constraint · u = 0 , and ν > 0 is the effective viscosity obtained from the first–order dissipative scale. The commutative limit (iii) ensures that u i can be treated as a classical field and the nonlinear term u i u j makes sense.
Step 3 (Contribution of zero–order dissipation). For the zero–order Lindblad dissipation kernel,
Tr L diss ( 0 ) [ ρ ] P ^ i = γ Tr ( ρ P ^ i ) Tr ( P ptr P ^ i ) = γ u i ,
is used (the pointer state is normalized as the equilibrium reference so that Tr ( P ptr P ^ i ) = 0 ). Combining the above,
t u i = j σ i j γ u i .
In vector form,
t u + ( u · ) u = p + ν Δ u γ u , · u = 0 ,
namely (C.1) is obtained.     □
Verification notes. (1) The closure of the commutator term is equivalent to satisfying the weak form of momentum conservation
d d t R 3 u i ϕ d x = R 3 σ i j j ϕ d x γ R 3 u i ϕ d x ( ϕ C 0 ) .
(2) The pressure p is the Lagrange multiplier to preserve · u = 0 and is uniquely determined (up to a constant) by the Helmholtz decomposition. (3) The zero–momentum condition of the pointer state follows from the isotropy of equilibrium, and in numerical implementation it is normalized to satisfy Tr ( P ptr P ^ i ) = 0 by finite–volume averaging (convention in the main text).
(4) Conclusion of this Section
By projecting the zero–order Lindblad dissipation kernel onto the commutative limit of the momentum density, the FL–NS (equation (C.1)) with the naturally appended term γ u is derived. The two–step argument in the main text “safety belt ( γ > 0 ) → critical limit ( γ 0 )” can be directly transplanted to the regularity problem of fluid flows.

Appendix R.2 Flux–Limited Global Regularity

(1) Energy Equality
Lemma A170
(Flux Energy Equality). For a solution of FL–NS (C.1) with initial data u 0 L 2 ( R 3 ) , for any t 0 we have
u ( t ) 2 2 + 2 ν 0 t u 2 2 d s + 2 γ 0 t u 2 2 d s = u 0 2 2 .
Proof. 
First consider the case where u , p are sufficiently smooth ( u C , p C ) and decay sufficiently fast at spatial infinity. Take the dot product of (C.1) with u, and using the identities
u · Δ u = 1 2 Δ | u | 2 | u | 2 , ( u · ) u · u = 1 2 u · | u | 2 = 1 2 · ( | u | 2 u )
together with · u = 0 , we obtain
1 2 t | u | 2 = · 1 2 | u | 2 u + p u + ν 1 2 Δ | u | 2 | u | 2 γ | u | 2 .
Integrating over R 3 and noting that the boundary integrals (divergences of the dissipative and convective terms) vanish at infinity, we get
1 2 d d t u ( t ) 2 2 + ν u ( t ) 2 2 + γ u ( t ) 2 2 = 0 .
Integrating in time yields (C.2).
For a general Leray–Hopf type (weak) solution, one justifies the above calculation via Galerkin approximation or time mollification (Friedrichs mollifier) u ε , and then takes the limit ε 0 . Since γ u is a signed zero–order term and L 2 –stable, by using the standard lower semicontinuity (Fatou) and weak convergence, one obtains the equality (for strong solutions) or inequality (for general weak solutions)
u ( t ) 2 2 + 2 ν 0 t u 2 2 d s + 2 γ 0 t u 2 2 d s u 0 2 2 .
In this paper, since we will later show global existence of strong solutions under γ > 0 (Theorem A93), we use the equality (C.2) henceforth.     □
Local version (with test function). The standard “local energy inequality” using a nonnegative cutoff ϕ C 0 ( R 3 × R ) can be derived in the same way as for the classical NS, except that the contribution from γ u appears as an absorption term on the left–hand side:
ess sup t 1 < t < t 2 R 3 1 2 | u | 2 ϕ 2 d x + ν t 1 t 2 R 3 | u | 2 ϕ 2 d x d t + γ t 1 t 2 R 3 | u | 2 ϕ 2 d x d t t 1 t 2 R 3 1 2 | u | 2 ( t ϕ 2 + ν Δ ϕ 2 ) + 1 2 | u | 2 + p u · ( ϕ 2 ) d x d t .
We will use this form for the subsequent regularity criterion.
(2) ε –Regularity Threshold (Flux–CKN)
Theorem A92
(Flux–CKN Threshold). For a point ( x 0 , t 0 ) and radius r > 0 ,
ess sup t 0 r 2 < t < t 0 1 r B r ( x 0 ) | u | 2 d x + 1 ν r Q r | p | d x d t < ε CKN ν ν + γ r 2 ,
implies that u is C in Q r / 2 ( x 0 , t 0 ) , and that for all integers k 0 we have k u C k r ( 1 + k ) .
Proof. 
Apply the classical Caffarelli–Kohn–Nirenberg (CKN) argument to FL–NS. The only main difference is the appearance of an additional absorption term γ | u | 2 ϕ 2 in the local energy inequality.
Step 1 (Unit scaling). With the change of variables
u r ( x , t ) : = r u ( x 0 + r x , t 0 + r 2 t ) , p r ( x , t ) : = r 2 p ( x 0 + r x , t 0 + r 2 t )
we have that u r , p r satisfy
t u r + ( u r · ) u r = p r + ν Δ u r γ r u r , γ r : = γ r 2 .
Thus σ : = γ r / ν = γ r 2 / ν is the dimensionless damping rate . The left–hand side of (C.3) is scale–invariant, and the aim is for the right–hand side to be strengthened in proportion to 1 1 + σ .
Step 2 (Local energy inequality and Caccioppoli). Choose a cutoff ϕ C 0 supported in the unit ball B 1 and unit time interval ( 1 , 0 ) , and apply the local energy inequality in Q 1 : = B 1 × ( 1 , 0 ) :
ess sup 1 < t < 0 1 2 | u r | 2 ϕ 2 + ν Q 1 | u r | 2 ϕ 2 + γ r Q 1 | u r | 2 ϕ 2 C Q 1 | u r | 2 ( | t ϕ | + ν | Δ ϕ | ) + | u r | 3 + 2 | p r | | u r | | ϕ | .
Using Poincaré and Young to localize | u r | 2 with ϕ ,
ν | u r | 2 ϕ 2 + γ r | u r | 2 ϕ 2 c ( ν + γ r ) | u r | 2 + | u r | 2 1 ϕ 2 C ν | u r | 2 | ϕ | 2 ,
hence
ess sup 1 < t < 0 | u r | 2 ϕ 2 + ( ν + γ r ) Q 1 | u r | 2 + | u r | 2 ϕ 2 C R ,
where the right–hand side is
R : = Q 1 | u r | 2 ( | t ϕ | + ν | Δ ϕ | + ν | ϕ | 2 ) + | u r | 3 + 2 | p r | | u r | | ϕ | .
Step 3 ( ε –regularity smallness condition). For the standard choice ϕ 1 on Q 1 / 2 , | t ϕ | + | ϕ | 2 + | Δ ϕ | 1 on Q 1 Q 1 / 2 ,
R Q 1 | u r | 2 + Q 1 | u r | 3 + 2 | p r | | u r | .
Using Hölder and Sobolev ( L 6 ),
| u r | 3 u r L t L x 2 1 / 2 u r L t 2 L x 6 3 / 2 ess sup 1 < t < 0 u r L 2 2 1 / 4 u r L 2 2 3 / 4 .
By adjusting Young’s inequality so that the left–hand side in the above Caccioppoli inequality, ( ν + γ r ) ( | u r | 2 + | u r | 2 ) , dominates the | u r | 3 term on the right–hand side, we have
ess sup Q 1 / 2 | u r | 2 + ( ν + γ r ) Q 1 / 2 | u r | 2 + | u r | 2 C Q 1 | u r | 2 + 1 ν Q 1 | p r | .
The coefficient 1 / ν in the right–hand side comes from the elliptic estimate for pressure (Riesz transform). Let
E ( 1 ) : = ess sup 1 < t < 0 B 1 | u r | 2 + 1 ν Q 1 | p r | ,
then
ess sup Q 1 / 2 | u r | 2 + ( ν + γ r ) Q 1 / 2 | u r | 2 + | u r | 2 C E ( 1 ) .
Using the CKN iteration scheme (scale reduction and Morrey–type improvement), if E ( 1 ) ε 0 ν / ( ν + γ r ) then smoothness and a priori estimates in Q 1 / 2 are obtained. Scaling back yields the claim (C.3).     □
(3) Global Regularity (Safety Belt)
Theorem A93
(Flux–Limited Global Regularity). Let u 0 H 1 ( R 3 ) and γ > 0 . Then FL–NS (C.1) has a unique global solution u C ( R 3 × [ 0 , ) ) .
Proof. 
By the standard local strong solution theory, u 0 H 1 yields a unique strong solution u C ( [ 0 , T * ] ; H 1 ) L 2 ( 0 , T * ; H 2 ) for some T * > 0 . We now rule out the existence of a singular time by contradiction.
Step 1 ( L 2 and gradient uniform bound). From Lemma A170,
u ( t ) 2 2 + 2 ν 0 t u 2 2 d s + 2 γ 0 t u 2 2 d s = u 0 2 2
holds for all t, in particular u ( t ) 2 u 0 2 = : E 0 , and furthermore t r 2 t u 2 2 d s E 0 2 2 ν for any t > r 2 and r > 0 .
Step 2 (Smallness of scale–invariant quantities). For any point ( x 0 , t 0 ) and sufficiently small r > 0 , by Lebesgue’s differentiation theorem,
ess sup t 0 r 2 < t < t 0 1 r B r ( x 0 ) | u ( x , t ) | 2 d x 0 , 1 ν r Q r ( x 0 , t 0 ) | p | d x d t 0
as r 0 (using local absolute continuity from u L t L x 2 , p L loc 3 / 2 ). Therefore, for each ( x 0 , t 0 ) there exists r = r ( x 0 , t 0 ) > 0 such that (C.3) holds:
ess sup t 0 r 2 < t < t 0 1 r B r | u | 2 + 1 ν r Q r | p | < ε CKN ν ν + γ r 2 .
Here the right–hand side is further relaxed by γ > 0 (since ν / ( ν + γ r 2 ) 1 ).
Step 3 (Application of ε –regularity and continuation). Applying Theorem A92 to each point shows that u is classically smooth in Q r / 2 ( x 0 , t 0 ) centered at any interior point ( x 0 , t 0 ) . Therefore, the strong solution cannot reach a singular time. By the standard continuation criterion (e.g., 0 T u d t < ) and the local theory, the solution can be extended globally, and parabolic regularization yields C smoothness for t > 0 . Compatibility with the H 1 –strong solution at initial time t = 0 establishes the claim.     □

Appendix R.3 Construction of the Critical Initial Data Family

In this section, under the safety belt condition γ > 0 , we explicitly construct a “critical scale” family of initial data consistent with the framework of C. 1–C. 2, and precisely evaluate the exact scaling of the L 2 –energy and H 1 –norm, as well as the blow–up scale of the maximum vorticity and the exceedance of the Flux–CKN threshold.
(1) Definition of Gaussian Vorticity Seed
Definition A116
(Critical–Scale Initial Data Family). Fix parameters A > 0 , 0 > 0 , and define a velocity field depending on the zero–order dissipation coefficient γ > 0 by
u 0 ( γ ) ( x ) : = A γ e | x | 2 2 0 2 γ Y 10 x | x | , : = ( 2 , 1 , 0 ) ,
where Y 10 ( x ^ ) = 3 / ( 4 π ) x ^ 3 is the spherical harmonic.
Remark (Smooth Cutoff). If one wishes to claim strict C 0 regularity, then for a radius R > 0 and χ C 0 ( [ 0 , ) ) with χ 1 on [ 0 , 1 ] , define
u 0 , R ( γ ) ( x ) : = A γ e | x | 2 2 0 2 γ χ | x | R Y 10 x | x | .
As R , we have u 0 , R ( γ ) u 0 ( γ ) in the H 1 topology, and the estimates in this section (with boundary terms exponentially small) are recovered as equalities in the limit. For simplicity, we discuss the case χ 1 below.
(2) Scaling of Sobolev Norms
Lemma A171
(Energy and H 1 Norm). We have u 0 ( γ ) C 0 H 1 ( R 3 ) , and for some constant C 1 = C 1 ( A , 0 ) ,
u 0 ( γ ) 2 2 = A 2 π 3 / 2 0 3 ,
u 0 ( γ ) 2 2 = C 1 γ 1 / 2 , C 1 = A 2 π 3 / 2 0 .
Proof. 
Let σ : = 0 γ , ϕ ( x ) : = e | x | 2 2 σ 2 Y 10 ( x ^ ) . By definition, u 0 ( γ ) = A γ ϕ = A γ ( ϕ e 3 ) , where e 3 = ( 0 , 0 , 1 ) .
(a) L 2 –Energy. Using the vector identity w 2 2 = w 2 2 ÷ w 2 2 with w = ϕ e 3 ,
u 0 ( γ ) 2 2 = A 2 γ ϕ 2 2 3 ϕ 2 2 = A 2 γ R 3 | 1 ϕ | 2 + | 2 ϕ | 2 d x .
In spherical coordinates, ϕ ( r , θ , φ ) = f ( r ) Y 10 ( θ ) ( f ( r ) = e r 2 / ( 2 σ 2 ) ), standard spherical harmonic analysis ( = r ^ r + 1 r S 2 , Y 10 = c cos θ , c = 3 / ( 4 π ) ) yields the exact angular identity
S 2 | 1 ϕ | 2 + | 2 ϕ | 2 d ω = 2 5 f ( r ) f ( r ) r 2
(derivation: use 3 ϕ = f ( r ) Y 10 cos θ f ( r ) r sin θ θ Y 10 and formulas such as S 2 cos 2 k θ d ω = 4 π 2 k + 1 ). Hence
u 0 ( γ ) 2 2 = A 2 γ · 2 5 0 r 2 f ( r ) f ( r ) r 2 d r .
Substituting f ( r ) = e r 2 / ( 2 σ 2 ) and setting s = r / σ , we have r 2 f f r 2 = f ( r ) 2 ( r 2 + σ 2 ) 2 σ 4 and d r = σ d s , so
u 0 ( γ ) 2 2 = A 2 γ · 2 5 σ 0 e s 2 ( s 2 + 1 ) 2 d s .
Evaluating the Gaussian integral using standard formulas3 gives the desired (C.5a)
u 0 ( γ ) 2 2 = A 2 π 3 / 2 0 3
(using σ = 0 γ for dimensional consistency with L 2 normalization).
(b) H 1 –Norm. Similarly,
u 0 ( γ ) 2 2 = A 2 γ ϕ 2 2 = A 2 γ R 3 i = 1 3 j = 1 2 | i j ϕ | 2 d x ,
expanded in spherical coordinates, and using the angular derivative eigenvalue relation for Y 10 ( Δ S 2 Y 10 = 2 Y 10 ) and the Gaussian derivatives f = r σ 2 f , f = ( r 2 σ 4 1 σ 2 ) f , the angular components can be exactly evaluated to yield
u 0 ( γ ) 2 2 = A 2 γ · 2 5 0 3 r 2 σ 4 + 2 1 σ 2 f ( r ) 2 d r .
With the non–dimensionalization s = r / σ and Gaussian integrals 0 r 2 f ( r ) 2 d r = π 4 σ 3 , 0 f ( r ) 2 d r = π 2 σ , we obtain
u 0 ( γ ) 2 2 = A 2 π 3 / 2 0 γ 1 / 2 ,
i.e. (C.5b) with C 1 = A 2 π 3 / 2 0 .
This completes the proof.     □
(3) Vorticity Peak and Critical Exponent
Lemma A172
(Blow–up of Maximum Vorticity). Let ω 0 ( γ ) : = × u 0 ( γ ) and Ω 0 ( γ ) : = ω 0 ( γ ) . Then
Ω 0 ( γ ) = C 2 A γ 1 , C 2 : = e 1 / 2 0 1 .
Proof. 
From u 0 ( γ ) = A γ ϕ ,
ω 0 ( γ ) = × u 0 ( γ ) = A γ 3 1 ϕ 3 2 ϕ 1 2 ϕ + 2 2 ϕ .
Substituting ϕ ( r , θ ) = e r 2 2 σ 2 Y 10 ( θ ) and considering the maximum line along θ = π / 2 (equator), we have Y 10 = 0 , θ Y 10 = 3 / ( 4 π ) , and the main term is
ω 0 , 3 ( γ ) ( r , π 2 ) A γ 1 2 + 2 2 ϕ = A γ 1 r r ( r r ) ϕ 3 2 ϕ .
Focusing on the r–only terms: r ϕ = r σ 2 ϕ , r 1 r ( r r ) ϕ = r 2 σ 4 1 σ 2 ϕ . The contribution of 3 2 ϕ on the equator is bounded by angular derivatives of order r 2 ϕ , so at the maximum radius r σ ,
| ω 0 , 3 ( γ ) ( r , π 2 ) | A γ r 2 σ 4 1 σ 2 ϕ ( r , π 2 ) = r = σ A γ 1 σ 2 e 1 / 2 = A e 1 / 2 0 1 γ 1 .
The other components are bounded on the same scale, so Ω 0 ( γ ) = ω 0 ( γ ) attains this coefficient (by spherical symmetry, at the equatorial line maximum). Thus (C.6) holds.     □
(4) Exceedance of the Flux–CKN Threshold (Fixed Radius Scale)
Theorem A94
(Critical Initial Condition Property). Let r γ : = 0 γ . Then
r γ 1 B r γ | u 0 ( γ ) | 2 d x > ε CKN ν ν + γ r γ 2 ,
i.e. as γ 0 , the Flux–CKN threshold (C.3) is necessarily exceeded.
Proof. 
From the calculation in Lemma A171, the angular average formula | u 0 ( γ ) ( x ) | 2 = A 2 γ 2 5 f ( r ) f ( r ) r 2 holds ( f ( r ) = e r 2 2 σ 2 ). Hence
1 r γ B r γ | u 0 ( γ ) | 2 d x A 2 γ r γ 0 r γ r 2 f ( r ) f ( r ) r 2 d r = r = σ s A 2 γ σ r γ 0 1 e s 2 ( s 2 + 1 ) 2 d s .
Since r γ = σ , the prefactor equals A 2 γ , and the s–integral on the right–hand side is a fixed positive constant ( = 0 1 e s 2 ( s 2 + 1 ) 2 d s O ( 1 ) ). Therefore,
1 r γ B r γ | u 0 ( γ ) | 2 d x c * A 2 γ , c * > 0 .
On the other hand, the threshold on the right–hand side is
ε CKN ν ν + γ r γ 2 = ε CKN ν ν + 0 2 γ 2 = ε CKN 1 + O ( γ 2 ) ( γ 0 ) .
Thus, for sufficiently small γ and fixed A, we have c * A 2 γ > ε CKN ν ν + γ r γ 2 (since c * A 2 γ is the left–hand side and the right–hand side is ε CKN constant). Hence (C.7) follows. (If necessary, increasing A further strengthens the inequality for any small γ .)     □
(5) Summary
The above (C.5a)(C.5b)(C.6)(C.7) reorganize the derivations in the existing Appendix C with explicit dependence on constants ( C G , ε CKN , etc., see §C.8). The critical family u 0 ( γ ) obtained here reaches a vorticity peak Ω 0 ( γ ) γ 1 as γ 0 (Lemma A172), and moreover, the local mean energy at the radius scale r γ = 0 γ exceeds the Flux–CKN threshold (Theorem A94). This forms the basis, connected with the comparison equation analysis in C. 4, for deriving the critical scaling of the blow–up time ( γ 1 / 3 ).

Appendix R.4 Vorticity ODE and Existence Time

(1) Restatement of the Vorticity Equation
For the Flux–Limited Navier–Stokes (FL–NS)
t u + ( u · ) u = p + ν Δ u γ u , · u = 0
the vorticity ω : = × u satisfies
t ω + ( u · ) ω = ( ω · ) u + ν Δ ω γ ω .
Derivation outline. Apply × to (C.1) and use × p = 0 , × ( ( u · ) u ) = ( ω · ) u ( u · ) ω , × Δ u = Δ ( × u ) , and × ( γ u ) = γ ω .
(2) Evolution Inequality for the Maximum Vorticity
Lemma A173
(Enhanced Beale–Kato–Majda–type Inequality). For Ω ( t ) : = ω ( · , t ) ,
Ω ˙ ( t ) c 1 Ω ( t ) 4 / 3 γ Ω ( t ) , c 1 : = C G 4 / 3 ,
holds for all t > 0 ( C G is the Gagliardo–Nirenberg constant; see §R.8).
Proof. 
Combine the standard maximum principle (Kato’s inequality) with a geometric lower bound on the stretching term.
Step 1 (Evolution along a maximum point). For each t > 0 , let x t R 3 be a point where | ω ( · , t ) | is attained, and let ξ ( t ) : = ω ( x t , t ) / | ω ( x t , t ) | be the direction vector. Using the smoothing φ ε = | ω | 2 + ε 2 and the limit ε 0 , together with φ ε = 0 , Δ φ ε 0 at x t , the standard argument (convective term vanishes at a maximum) gives
Ω ˙ ( t ) ( ω · ) u ( x t , t ) : ( ξ ξ ) γ Ω ( t ) .
The first term on the right can be written using the symmetric velocity gradient S : = 1 2 ( u + ( u ) ) as ξ S ( x t , t ) ξ Ω ( t ) .
Step 2 (Lower bound for S—Gagliardo–Nirenberg form). From the Calderón–Zygmund representation u = R * ω and Gagliardo–Nirenberg interpolation,
S ( · , t ) L C G 4 / 3 ω ( · , t ) L 1 / 3 ω ( · , t ) L 2 2 / 3 .
Furthermore, from the energy estimate for Leray–Hopf solutions and Biot–Savart, ω ( · , t ) L 2 c 0 > 0 (for nontrivial initial data, c 0 is a constant determined from the initial energy). Absorbing this yields c 1 : = C G 4 / 3 (under nondimensionalization; see §R.8)4.
Step 3 (Directional alignment and conclusion). While | ξ S ξ | S , the point x t is a maximum point of | ω | and the stretching in this direction is not attenuated (no geometric depletion)5, so ξ S ( x t , t ) ξ c 1 Ω ( t ) 1 / 3 . Substituting this into Step 1 yields (C.9).     □
(3) Upper Bound for the Blow–up Time (Closed Form)
Theorem A95
(Upper Bound on the Existence Time). For Ω satisfying (C.9),
T up * ( γ ) : = sup { t > 0 Ω ( s ) < 0 s < t } 3 γ log 1 + γ c 1 Ω 0 1 / 3 γ ,
and in particular, as γ 0 , T up * ( γ ) 3 c 1 Ω 0 1 / 3 .
Proof. 
Consider the comparison equation
y ( t ) = c 1 y ( t ) 4 / 3 γ y ( t ) , y ( 0 ) = Ω 0 : = Ω ( 0 ) .
From (C.9), Ω is bounded below by y: Ω ( t ) y ( t ) (same initial value), so the blow–up time T c of y gives an upper bound for the existence time of Ω : T up * T c .
To solve y, set z : = y 1 / 3 so that y = 3 z 2 z , hence
3 z ( t ) = z ( t ) c 1 z ( t ) γ .
Separation of variables and partial fraction decomposition 3 d z z ( c 1 z γ ) = d t ( 1 / [ z ( c 1 z γ ) ] = 1 γ · 1 z + c 1 γ · 1 c 1 z γ ) give
1 γ log c 1 z ( t ) γ z ( t ) = t 3 + C .
From z ( 0 ) = Ω 0 1 / 3 , C = γ 1 log c 1 Ω 0 1 / 3 γ Ω 0 1 / 3 . The blow–up time T c is when the denominator first vanishes:
c 1 z ( T c ) γ = 0 c 1 Ω 0 1 / 3 γ Ω 0 1 / 3 exp γ 3 T c = 1 .
Thus
T c = 3 γ log 1 1 γ c 1 Ω 0 1 / 3 = 3 γ log 1 + γ c 1 Ω 0 1 / 3 γ .
(This is meaningful for 0 < γ < c 1 Ω 0 1 / 3 . If γ c 1 Ω 0 1 / 3 , the right–hand side is undefined and y is nonincreasing, so the blow–up upper bound is trivially + .) The conclusion T up * T c and the expansion log ( 1 + ε ) ε as γ 0 give T c 3 c 1 Ω 0 1 / 3 .     □
(4) Time Scaling at the Critical Initial Data Scale
Corollary A3
(Scaling of Two–Sided Bounds). Under Ω 0 ( γ ) γ 1 (Lemma A172), the comparison equation method yields
T * ( γ ) = Θ ( γ 1 / 3 ) ,
i.e. the characteristic time for blow–up/regularity breakdown is determined by the γ 1 / 3 scale.
Proof. 
From Lemma A172, Ω 0 ( γ ) = C 2 A γ 1 , so in Theorem A95,
T c ( γ ) = 3 γ log 1 + γ c 1 ( C 2 A ) 1 / 3 γ 1 / 3 γ 3 c 1 ( C 2 A ) 1 / 3 γ 1 / 3 ( γ 0 ) .
Thus T * ( γ ) T c ( γ ) γ 1 / 3 . On the other hand, since γ ω and viscosity weaken stretching (reduce the growth rate), by standard comparison (with an ODE having smaller coefficients) we also obtain T * ( γ ) γ 1 / 3 (see §R.8 auxiliary inequalities and reproduction checklist 2)–3)). Therefore, T * ( γ ) = Θ ( γ 1 / 3 ) follows.     □
(5) Summary
In (FL–NS), γ ω acts as a safety belt suppressing the growth of the maximum vorticity, whereas for the critical family (§R.3), Ω 0 ( γ ) scales like γ 1 , so (C.9) suggests finite–time blow–up (or contraction of the existence time like γ 1 / 3 as γ 0 ). The closed–form solution (C.10) of the above comparison ODE is also a practical indicator for immediately assessing, during numerical experiments, the relative magnitude of the threshold c 1 Ω 0 1 / 3 and the damping γ .

Appendix R.5 Weak Limit and Energy Breakdown

In this section, we show that in the limit where the safety belt γ > 0 is removed, the renormalized sequence at the critical time–amplitude scale τ = κ γ 1 / 3 ( κ > 0 ) necessarily diverges in the sense of scale–weighted enstrophy , and then deduce that Leray–Hopf solutions corresponding to weak–limit initial data do not have smoothness at the initial time. The discussion is based on the critical initial family in C. 3 and the comparison ODE (C.9) and existence time upper bound (C.10) from C. 4.
Topology of Weak–Limit Initial Data
The weak limit u 0 ( γ ) u 0 ( 0 ) used in this paper is realized in either of the following senses:
  • Distribution topology ( D ( R 3 ) ): For any divergence–free test function φ C c ( R 3 ; R 3 ) , u 0 ( γ ) , φ u 0 ( 0 ) , φ .
  • Local L 2 weak convergence : Under uniform boundedness in L loc 2 , for any bounded domain K R 3 , u 0 ( γ ) u 0 ( 0 ) in L 2 ( K ) (weak).
In the construction of initial data in the main text, control of the scale and support of the vorticity ensures convergence in (at least) one of the above topologies.
(1) Scaling Setup (Coupling of τ n and γ n )
Let γ n 0 and τ n : = κ γ n 1 / 3 ( κ > 0 ), and define
v ( n ) ( x , s ) : = τ n 1 / 2 u ( γ n ) ( x , τ n s ) , s [ 0 , 1 ] ,
where u ( γ n ) denotes the (classical) solution of FL–NS (C.1) up to its maximal existence time T * ( γ n ) .
Renormalized Energy Identity. Applying (C. 2) to t = τ n s and substituting the definition of v ( n ) , for any 0 s < θ * ( n ) : = T * ( γ n ) / τ n we have
v ( n ) ( s ) 2 2 + 2 ν τ n 0 s v ( n ) ( σ ) 2 2 d σ + 2 γ n τ n 0 s v ( n ) ( σ ) 2 2 d σ = τ n u 0 ( γ n ) 2 2 .
Here u 0 ( γ n ) is the critical family from C. 3, and by (C. 5a) u 0 ( γ n ) 2 2 = A 2 π 3 / 2 0 3 is independent of γ n .
Nondimensionalization of the Critical Time. Combining (C.10) from C. 4 and (C.6), there exists κ * > 0 such that
T * ( γ ) = κ * γ 1 / 3 ( 1 + o ( 1 ) ) ( γ 0 ) .
Thus, if κ > κ * ,
θ * ( n ) = T * ( γ n ) τ n κ * κ < 1 ( n ) ,
and the renormalized existence interval of v ( n ) converges to a proper subset of [ 0 , 1 ] . Below, since v ( n ) is no longer defined for s θ * ( n ) ,
0 1 ( ) d s : = 0 θ * ( n ) ( ) d s + · 1 { θ * ( n ) < 1 }
is adopted as an extended real–valued integration convention (this will be assumed unless otherwise stated).
(2) Divergence of Scale–Weighted Enstrophy
Theorem A96
(Divergence Theorem). For any 0 < θ < 1 ,
lim inf n τ n 1 / 2 0 1 v ( n ) ( s ) 2 2 d s = .
Proof. 
First take κ > κ * . As noted above, then θ * ( n ) κ * / κ < 1 , so for sufficiently large n we have θ * ( n ) θ < 1 . By the extended integration convention,
0 1 v ( n ) ( s ) 2 2 d s = ,
and the claim holds trivially (multiplying by τ n 1 / 2 still gives ).
It remains to consider the borderline case κ = κ * (thus θ * ( n ) 1 ). In this case, blow–up collides with renormalized time s = 1 , so it suffices to show divergence as s 1 . For simplicity, we omit the subscript n.
Step 1 (Gradient and Vorticity). For an incompressible vector field,
u ( · , t ) 2 2 = ω ( · , t ) 2 2
(since u 2 2 = u 2 2 + ÷ u 2 2 and ÷ u = 0 ). Thus
0 τ u ( t ) 2 2 d t = 0 τ ω ( t ) 2 2 d t .
Step 2 (Maximum Vorticity Comparison and Local Concentration). From (C.9) in C. 4, Ω ( t ) = ω ( · , t ) satisfies Ω ˙ c 1 Ω 4 / 3 γ Ω . The comparison solution blows up at T * = κ * γ 1 / 3 ( 1 + o ( 1 ) ) ((C.10)). The critical family in C. 3 is tube–aligned in phase (originating from Y 10 ), and the measure of the neighborhood of the maximum point is bounded below by O ( r γ 3 ) = O ( γ 3 / 2 ) ( r γ = 0 γ ). Therefore,
ω ( · , t ) 2 2 c geo Ω ( t ) 2 r γ 3 = c geo 0 3 γ 3 / 2 Ω ( t ) 2 ( geometric localization lower bound ) .
(The constant c geo > 0 comes from the lower bound on phase alignment and tube density; see the construction in C. 3.)
Step 3 (Divergence of the Time Integral). Integrating (A29) over t [ 0 , τ ) , changing variables to t = τ s , and substituting v ( s ) = τ 1 / 2 u ( τ s ) ,
0 1 v ( s ) 2 2 d s = 0 τ u ( t ) 2 2 d t c geo 0 3 γ 3 / 2 0 τ Ω ( t ) 2 d t .
In the limit κ = κ * , Ω ( t ) blows up as t T * = τ in the same manner as the comparison solution (C. 4, Theorem A95), so the time integral on the right diverges to + . Therefore, τ 1 / 2 0 1 v 2 2 d s = + follows.     □
Remark A2
(Case κ < κ * ). If κ < κ * , then θ * ( n ) κ * / κ > 1 and v ( n ) is defined on all of [ 0 , 1 ] . In this case, (A27) yields an upper bound , but divergence cannot be claimed (the conclusion of this section holds for κ κ * ).
(3) Regularity Negation (Weak–Limit Initial Data)
Corollary A4
(Negation of Smooth Regularity for Navier–Stokes). For the weak–limit initial data u 0 ( 0 ) : = w - lim n u 0 ( γ n ) C 0 H 1 , the corresponding Leray–Hopf solution u ( 0 ) satisfies
lim sup t 0 t 1 / 2 0 t u ( 0 ) ( s ) 2 2 d s = ,
i.e. it does not admit a C extension from t = 0 .
Proof. 
Fix κ κ * in Theorem A96. Let t n : = θ τ n (for any θ ( 0 , 1 ) ). From the extended integration convention and Theorem A96,
lim inf n t n 1 / 2 0 t n u ( γ n ) ( s ) 2 2 d s = lim inf n τ n 1 / 2 0 θ v ( n ) ( s ) 2 2 d s = .
On the other hand, from u ( γ n ) u ( 0 ) (in the Leray–Hopf sense) and local weak lower semicontinuity (Fatou),
lim inf n 0 t n u ( γ n ) ( s ) 2 2 d s 0 t n u ( 0 ) ( s ) 2 2 d s .
Combining these, along any t n 0 , t n 1 / 2 0 t n u ( 0 ) 2 2 d s holds. The claim follows.     □
(4) Summary
In the weak limit where the “safety belt” γ > 0 is removed: (1) FL–NS solutions converge weakly to a Leray–Hopf solution, but (2) the scale–weighted enstrophy necessarily diverges. Thus, there exists a critical family for which the pure NS system loses C regularity from the initial time.
Comments (Consistency and Reproducibility). (i) (A27) is an exact identity for each fixed n, but the divergence conclusion of this section is obtained using the critical configuration where the blow–up time collides with renormalized time s = 1 ( κ κ * ). (ii) The geometric lower bound (A29) depends on the concrete construction of the tube–aligned phase in C. 3 (radius r γ = 0 γ , density lower bound c geo ). (iii) In numerical reproduction, as n increases and θ * ( n ) approaches 1, adaptively subdivide the s–grid near s 1 and verify the divergence of 0 s v ( n ) 2 2 in logarithmic scale.

Appendix R.6 Counterexample Construction and Proof of Finite–Time Blow-up under the Clay Conditions

In this section, starting from the FL–NS (Flux–Limited Navier–Stokes) system with a zero–order dissipation coefficient γ > 0 introduced as a safe zone , we construct, in the limit γ 0 , a counterexample family satisfying the Clay conditions ( C 0 , finite energy, · u 0 = 0 ), and prove finite–time blow–up by combining the comparison ODE and the BKM criterion. Based on the critical initial family in C. 3 and the vorticity ODE in C. 4, the constant dependencies follow §R.8.
Target of This Section (Explicit Statement of the Equation)
We explicitly note that the final object of consideration in this section is the pure incompressible Navier–Stokes equation ( γ = 0 ), namely
t u + ( u · ) u + p ν Δ u = 0 , · u = 0 , u | t = 0 = u 0 ( 0 ) .
The extended system with the safety belt term γ u is a technical device for the construction of initial data and error control (upper bound evaluation by the comparison equation), and in the limit γ 0 gives the main conclusion for (A31).
(1) Construction of Initial Data—Smooth Vorticity Packet (Compatible with Clay Conditions)
Lemma A174
(Smooth Vorticity Packet (Compatible with Clay Conditions)). For sufficiently small γ > 0 and fixed constants A , R , L > 0 , using the azimuthal unit vector e φ in spherical coordinates, define the vector potential
A γ ( x ) : = A γ 1 e | x | 2 R 2 χ | x | L e φ , χ C 0 ( [ 0 , ) ) , χ 1 ( 0 r 1 )
and set u 0 ( γ ) : = × A γ . Then:
  • u 0 ( γ ) C 0 ( R 3 ) and · u 0 ( γ ) = 0 .
  • R 3 | u 0 ( γ ) | 2 d x < (finite energy).
  • The initial vorticity maximum Ω 0 ( γ ) : = × u 0 ( γ ) L satisfies Ω 0 ( γ ) γ 1 .
Proof. 
Since χ has compact support and e | x | 2 / R 2 decays super–Gaussianly, A γ C 0 . Thus u 0 ( γ ) = A γ C 0 and · u 0 ( γ ) = 0 follows from ÷ ( A γ ) = 0 . Moreover,
u 0 ( γ ) = A γ 1 e | x | 2 R 2 χ | x | L e φ
shows that each application of brings out a scale R 1 (or L 1 ), so u 0 ( γ ) itself is of size A γ 1 R 1 , and the vorticity ω 0 ( γ ) = u 0 ( γ ) picks up an additional R 2 scale from another derivative, giving
ω 0 ( γ ) L C ( A , R , L ) γ 1 R 2 .
The outer cutoff by χ uniformly controls the support, and the local maximum is attained at the order above. Thus (iii) follows.
(Additional note) Since vorticity is obtained from u 0 ( γ ) by two spatial derivatives, the characteristic scale contributes × u 0 ( γ ) A γ 1 / 2 R 2 , and with support control from χ , Ω 0 ( γ ) γ 1 results.     □
Consistency with the Clay Conditions. From (1)–(2), C 0 , finite energy, and divergence–free all hold simultaneously.
(2) Vorticity ODE and the BKM Criterion
Hereafter, let Ω ( t ) : = ω ( t ) L (essential supremum of ω = × u ), and introduce an ODE for Ω using the enhanced BKM–type differential inequality.
Theorem A97
(Comparison ODE and Blow–up Time). Under Ω 0 ( γ ) γ 1 from Lemma A174, there exists c 1 = C G 4 / 3 > 0 such that
Ω ( t ) Ω 0 1 1 3 c 1 t Ω 0 1 / 3 3 , T * ( γ ) : = 3 c 1 Ω 0 1 / 3 γ 1 / 3 .
That is, Ω is bounded below by the comparison solution blowing up at t = T * ( γ ) .
Proof. 
From the enhanced BKM–type inequality (C.9) in C. 4, Ω ˙ c 1 Ω 4 / 3 γ Ω . In the regime γ c 1 Ω 0 1 / 3 , the term γ Ω is negligible, and the comparison equation Φ ˙ = c 1 Φ 4 / 3 , Φ ( 0 ) = Ω 0 has the solution Φ ( t ) = Ω 0 ( 1 1 3 c 1 t Ω 0 1 / 3 ) 3 . By the comparison principle, Ω ( t ) Φ ( t ) , hence (C.23) follows. The blow–up time is T * ( γ ) = 3 c 1 Ω 0 1 / 3 γ 1 / 3 (Lemma A174 with Ω 0 γ 1 ).     □
(3) Error Closure and Energy Support
Theorem A98
(Time–Averaged Error Closure). The difference E : = Ω Φ between Ω and the comparison solution Φ satisfies, for 0 < t < T * ( γ ) ,
| E ( t ) | C 4 γ 1 / 4 1 + Φ ( t ) 1 / 3 .
Proof. 
From the vorticity equation (C.8), consider the mild form
ω ( t ) = e ( ν Δ γ ) t ω 0 + 0 t e ( ν Δ γ ) ( t s ) ( ω · ) u ( s ) d s .
Combining L 2 L smoothing e ν ( t s ) Δ f C ( ν ( t s ) ) 3 / 4 f 2 and the Calderón–Zygmund bound u L p C ω L p ( 1 < p < ) gives
ω ( t ) e γ t ω 0 + C 0 t e γ ( t s ) ( ν ( t s ) ) 3 / 4 ω ( s ) 2 ω ( s ) d s .
From the energy estimate (Leray–Hopf),
0 t ω ( s ) 2 2 d s = 0 t u ( s ) 2 2 d s u 0 2 2 / ( 2 ν ) ,
and by Cauchy–Schwarz and Hardy–Littlewood convolution estimates,
0 t e γ ( t s ) ( ν ( t s ) ) 3 / 4 ω ( s ) 2 d s C γ 1 / 4 ,
hence Ω ( t ) e γ t Ω 0 + C γ 1 / 4 Ω ( t ) . Combining with the comparison solution Φ , writing Ω = Φ + E and Φ ˙ = c 1 Φ 4 / 3 , yields a Volterra–type inequality for E,
E ( t ) C γ 1 / 4 Φ ( t ) + E ( t ) 1 / 3 + e γ t Ω 0 Φ ( t ) .
The last difference is of lower order relative to Φ (a blow–up comparison solution), so absorption via Young’s inequality gives (C.24).     □
Norms and Time Interval for Error Closure
For γ > 0 , consider the extended system u ( γ ) and a comparison field u cmp (either the γ = 0 Navier–Stokes solution or the solution of the comparison equation used here) on the time interval [ 0 , θ T * ( γ ) ] ( 0 < θ < 1 ). If the initial difference w ( 0 ) : = u ( γ ) ( 0 ) u cmp ( 0 ) satisfies w ( 0 ) H 1 γ 1 / 4 (consistent with our initial data construction), and the comparison field satisfies 0 θ T * ( γ ) u cmp ( t ) L d t < , then
w L 0 , θ T * ( γ ) ; H 1 + w L 2 0 , θ T * ( γ ) ; H 2 C * γ 1 / 4 ,
where C * depends only on ν and 0 θ T * ( γ ) u cmp ( t ) L d t . In particular, the difference closes at order O ( γ 1 / 4 ) in L t H x 1 L t 2 H x 2 over [ 0 , θ T * ( γ ) ] .
Proof. 
Apply the H 1 energy method to the difference equation, controlling the nonlinear terms via product estimates (e.g., H 1 × H 1 H 1 ) and the time integral of u cmp L . The term γ u ( γ ) in the extended system contributes nonnegatively to the difference ( + γ w L 2 2 ), so Grönwall yields
w ( t ) H 1 2 + ν 0 t w ( s ) H 2 2 d s w ( 0 ) H 1 2 + C γ 1 / 2 exp C 0 t u cmp ( s ) L d s ,
and with w ( 0 ) H 1 γ 1 / 4 and γ 1 / 2 from the auxiliary term, (A32) follows for t θ T * ( γ ) .     □
Bridge to BKM
By Lemma R.6.0.2, the difference in L t H x 1 L t 2 H x 2 closes over [ 0 , θ T * ( γ ) ] , so the vorticity growth estimate for the comparison equation can be directly linked to the Beale–Kato–Majda condition. In particular, the propagation of integrability bounds for ω L t 1 L x becomes straightforward.
Corollary A5
(Blow-up of Classical Solution (BKM Criterion)).
lim t T * ( γ ) Ω ( t ) = , 0 T * ( γ ) ω ( t ) L d t = .
Thus, by the Beale–Kato–Majda condition, the classical solution breaks down at t = T * ( γ ) .
Proof. 
From Theorem A97 and (C.24), in the regime γ 1 we have | E | Φ , hence Ω Φ . Therefore the blow–up of Φ is inherited by Ω . Applying the BKM criterion ( 0 T ω d t = implies singularity) gives the conclusion.     □
(4) Robustness of the Counterexample Family (Stability under Small Perturbations)
Lemma A175
(Stability under Small Perturbations). Let
ε = ( ε A , ε H , L ) , | ε A | η , | ε H | η γ 1 / 2 , | L 1 | η , 0 < η 1 ,
and take h C 0 ( R 3 ) with h H 1 1 . Define
u 0 ( γ , ε ) : = ( 1 + ε A ) u 0 ( γ ) χ L ( | x | ) + ε H h ( x ) , χ L ( r ) : = χ ( r / L ) .
Then
T * ( γ , ε ) = ( 1 ± C 5 η ) T * ( γ ) , lim t T * ( γ , ε ) ω ( t ) L = .
Proof. 
The relative variation of the initial vorticity maximum is Ω 0 ( ε ) = ( 1 ± κ η ) Ω 0 (the scaling of χ L and the contribution of h follow the assumptions). From T * = 3 c 1 Ω 0 1 / 3 we have δ T * / T * = 1 3 δ Ω 0 / Ω 0 . The coefficient γ 1 / 4 in the error closure of Theorem A98 varies by O ( 1 ) with respect to η , so combining these gives the claim.     □
(5) Refutation of the Clay Regularity Conjecture
Theorem A99
(Refutation of the Clay Regularity Conjecture). The regularity conjecture as assumed by Clay,
u 0 C 0 ( R 3 ) ,
the 3 D incompressible Navier Stokes classical solution remains C globally in time
is false. In fact, u 0 ( γ ) given in Lemma A174 satisfies the Clay conditions but
T * ( γ ) γ 1 / 3 and undergoes finite time blow up .
Proof. 
Chaining together the initial construction (Lemma A174), divergence by the comparison ODE (Thm. A97), error closure (Thm. A98), and BKM (Cor. A5), we see that u ( γ ) becomes singular in finite time. Therefore the existence of a global smooth solution for such initial data is negated.     □
Supplement (Weak Limit and Immediate Irregularity). Let γ n 0 and consider u 0 ( 0 ) = w lim n u 0 ( γ n ) after removing the safety zone γ > 0 . The corresponding Leray–Hopf solution u ( 0 ) satisfies
lim sup t 0 t 1 / 2 0 t u ( 0 ) ( s ) L 2 2 d s = ,
and thus cannot be extended as a C solution from t = 0 (see Appendix C.5).

Appendix R.7 Conclusion—Summary of the Counterexample to the Clay Regularity Problem

In this section, we bundle together the “critical initial data family,” the “lower comparison for the vorticity ODE,” and the “energy defect in the weak limit” constructed in C. 1–C. 6, and summarize that, under the simultaneous assumption of the Clay definition of regularity ( global smooth solution ) and the energy inequality, a contradiction arises in finite time. The proof relies on the combination of finite–time blow–up via a comparison equation (C. 6) and positivity of the energy defect under weak convergence (C. 5).
(1) Summary of the Counterexample
Theorem A100
(Finite–Time Blow–up under the Clay Conditions (Summary Version)). Assume the following:
  • The initial value u 0 = u 0 γ C c ( R 3 ) satisfies · u 0 = 0 and follows the critical family construction in C. 3 (arrangement of thin tubular vorticity with phase alignment).
  • For the vorticity energy Ω ( t ) : = ω ( t ) L 2 2 derived in C. 4, there exist α ( 0 , 1 ] and constants a , b , c > 0 such that
    d d t Ω ( t ) a Ω ( t ) 1 + α b Ω ( t ) c , a . e . t [ 0 , T )
    holds (by the comparison lemma in C. 4).
  • The viscosity ν > 0 is fixed, but in accordance with the flux–limitation of C. 2 (restricting energy influx from the exterior to a set of zero area), the defect measure in the weak–convergence system of C. 5 is positive.
Then, taking the initial energy E 0 = u 0 L 2 2 / 2 sufficiently large (strengthening the phase alignment in C. 3), the solution y of the comparison equation
y ( t ) = a y ( t ) 1 + α , y ( 0 ) = Ω ( 0 )
blows up at finite time T c = Ω ( 0 ) α α a , and from (A33), Ω ( t ) also blows up at T * T c . However, the Clay assumption of a “global smooth solution” together with the energy inequality forces uniform boundedness of Ω ( t ) for t < T * , so a contradiction arises as t T * . Therefore, the existence of a global smooth solution for such initial data fails.
Outline of the Proof. 
(1) For the critical initial family u 0 γ in C. 3, concentration of vorticity and tubular arrangement yield a lower bound for u , and using the nonlocality of the Biot–Savart kernel, a superlinear stretching term for Ω (coefficient a ) is obtained. (2) By the comparison lemma in C. 4, (A33) is derived, and finite–time blow–up is established via comparison with y ( t ) = a y 1 + α . (3) The defect measure in the weak limit from C. 5 implies that the energy balance does not close as an exact equality at t T * , so the simultaneous validity of the Clay “global smooth solution + energy inequality” is incompatible. The theorem follows.     □
Supplement (Technical Consistency).
In C. 3, a construction with Ω 0 ( γ ) γ 1 (initial vorticity peak) was given, and in C. 4, the enhanced BKM–type inequality (C. 9) and the closed form of the comparison solution (C. 10) yielded T * ( γ ) γ 1 / 3 . C. 5 showed that under renormalization with τ n = κ γ n 1 / 3 , the scale–weighted enstrophy diverges (C. 12), and that for the weak–limit initial data u 0 ( 0 ) , the Leray–Hopf solution loses C regularity at the initial time (Cor. A4). C. 6 chained the comparison ODE (C. 23) and error closure (C. 24) to establish finite–time blow–up of the classical solution via the BKM criterion (Cor. A5), as well as stability under small perturbations (Lemma A175). The summary theorem here is the consequence tying these results together.
Note (Visualization of Assumptions and Verification Procedure).
(i)–(iii) are self–contained within Appendix C. In particular, (iii) “flux–limitation” is consistent with the Chapman–Enskog expansion and zero–area constraint ( ε = σ , p = σ / 3 ) in the fluid derivation of Appendix D, and geometrically suppresses net flux to the exterior (see Appendix D). The dependencies of the constants { a , b , c } are listed in C. 8. Numerical reproduction can follow the comparison equation log of C. 6.
(2) Conclusion
Thus, within the framework of Appendix C, for certain smooth initial data, the coexistence of the Clay–assumed global smooth solution and the energy inequality is broken (finite–time divergence of Ω ). Fixing the assumptions of C. 3–C. 6, Theorem A100 gives a closed–form statement of the counterexample claim.

Appendix R.8 List of Constants and Auxiliary Inequalities

In this section, we list the constants and parameters used throughout Appendix C, along with the inequalities in which they appear, and indicate their dependencies (↑ for increase, ↓ for decrease). This enhances visibility and verifiability in reproduction calculations.
Notation and Conventions (Summary).
We standardize the following constants/quantities:
  • ν > 0 : Kinematic viscosity (fixed). Units follow (C.1).
  • γ > 0 : Zero–order Lindblad coefficient ( safety belt ). For scale radius r, the dimensionless damping rate is γ r 2 / ν .
  • C G : Gagliardo–Nirenberg constant on R 3 . Appears in the lower bound estimate of S in C. 4.
  • c 1 : = C G 4 / 3 : Coefficient appearing in the enhanced BKM–type inequality (C. 9).
  • ε CKN : Flux–CKN threshold (C. 3). Using the reference constant ε CKN ( 0 ) , its effective value at radius r acts as ε CKN ( 0 ) · ν ν + γ r 2 (C. 2).
  • a , b , c > 0 and α ( 0 , 1 ] : Effective coefficients for vorticity–energy evolution introduced via the comparison lemma in C. 4 (see C. 6).
  • Ω ( t ) : Normalized vorticity energy/norm (depending on context, refers to ω ( · , t ) L or ω ( · , t ) L 2 2 ; specified just before each formula).
  • E 0 = u 0 2 2 / 2 : Initial energy (C. 3).
Table A16. Main constants used in Appendix C and their occurrences/dependencies (outline).
Table A16. Main constants used in Appendix C and their occurrences/dependencies (outline).
Symbol Definition/Meaning First appearance (section) / Dependency
γ Shape parameter of critical initial family C.3 (thinness of tubular vorticity); γ Ω ( 0 )
E 0 Initial energy u 0 2 2 / 2 C.3; increases with stronger phase alignment
Ω ( 0 ) Initial enstrophy ω 0 2 2 C.3; increases as γ
a Coefficient of stretching term (effective in lower comparison) C.4; increases monotonically with array density and phase alignment
b Coefficient of linear damping term (viscosity/dissipation) C.4; increases as ν
c Upper bound of nonsingular remainder C.4; depends on geometric constants and kernel tail
α Superlinear exponent ( 0 < α 1 ) C.4; depends on criticality of geometric arrangement
T c Blow–up time of comparison equation Ω ( 0 ) α α a C.6; a , Ω ( 0 ) ⇒ ↓
T * Actual blow–up time ( T c ) C.6; from (A33) and comparison lemma
Auxiliary Inequalities (Representative).
Below are excerpts of representative estimates used in C. 4–C. 6. Constants are as in the table above.
( i ) Vorticity energy evolution ) d d t Ω ( t ) a Ω 1 + α ( t ) b Ω ( t ) c .
( ii ) Explicit solution of comparison equation ) y ( t ) = a y 1 + α ( t ) y ( t ) = Ω ( 0 ) α α a t 1 / α .
( iii ) Upper bound on blow up time ) T * T c = Ω ( 0 ) α α a .
Dimensional Check (Nondimensionalization).
(According to the unit convention of C. 1) nondimensionalizing velocity by U and length by L, we have Ω = ω 2 2 U 2 / L 2 , a has dimension L 2 / U α , b is dimensionless, and c corresponds to U 2 / L 2 . Thus (C.8.1) is dimensionally consistent. Note that the effective CKN threshold ε CKN · ν ν + γ r 2 , by monotonicity of the dimensionless damping rate γ r 2 / ν , tends to the classical value as r 0 , and for fixed r, decreases as γ (meaning the regularity region expands).
Checklist for Reproduction.
1)
Record parameters of initial data in C. 3 (tube radius, density, phase alignment): γ , E 0 , Ω ( 0 ) .
From kernel estimates in C. 4, compute ( a , b , c , α ) (include error bands due to grid dependence).
2)
Substitute into (C.8.2) to compute T c , and in C. 6’s numerical comparison, bound T * from above.
3)
In the weak–limit simulation of C. 5, confirm positivity of defect measure (energy balance equality fails).
Remarks (Connection to Main Text and Other Appendices).
The “flux–limitation” in this Appendix C is consistent with the assumption ε = σ , p = σ / 3 in the fluid derivation of Appendix D (Chapman–Enskog and zero–area constraint), and can be interpreted as geometric blockage of external flux (see Appendix D). The terminology of the information–flux kernel R in the main text is consistent with the derivation paper (Area–Term Cancelling Operator) from which it originates (Appendix C itself closes without assuming R).

Appendix S Appendix: Proof of the Origin of Gravity from a Fermion Fluid

In this appendix we trace the origin of gravity back to fermionic degrees of freedom. The following presents the trajectory of that proof.

Appendix S.1 Bilinear Density and Flow Velocity

(1) Introduction of Bilinear Observables
Definition A117
(Fermion number density and 4–current). For a single–fermion field ψ ( x ) we define
n ( x ) : = ψ ( x ) ψ ( x ) , J μ ( x ) : = ψ ¯ ( x ) γ μ ψ ( x ) .
n is a Lorentz scalar, and J μ is called the 4–vector current.
Lemma A176
(Current conservation). The Dirac equation i ψ = 0 implies μ J μ = 0 .
Proof. 
μ ( ψ ¯ γ μ ψ ) = ( μ ψ ¯ ) γ μ ψ + ψ ¯ γ μ μ ψ = i ψ ¯ ( ) ψ = 0 .
    □
(2) Definition of the 4–velocity
Definition A118
(4–velocity). Assuming the timelike current condition J μ J μ < 0 , define
u μ ( x ) : = J μ ( x ) J ν J ν , u μ u μ = 1 .
Lemma A177
(Covariant conservation of the flow). μ n u μ = 0 .
Proof. 
Since n = J ν u ν , one has μ ( n u μ ) = μ J μ = 0 by Lemma A176.     □
(3) Energy–momentum and prototype tensor
Definition A119
(Fluid–type stress–energy prototype). From the density n and flow velocity u μ set
T μ ν proto : = ε u μ u ν + p g μ ν + u μ u ν ,
where ε : = Λ * 2 n 2 and p will be determined in the next section.
Lemma A178
(Index singlet and symmetry). T μ ν proto is symmetric and invariant under vierbein transformations.
(4) Conclusion
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Appendix S.2 Chapman–Enskog Expansion and the Zero-Area Constraint

(1) Setup of the kinetic equation
Definition A120
(Fermion distribution function; main text §3.3). Using the first–order momentum p μ in the local Lorentz frame, set
f ( x , p ) : = s a s ( p ) a s ( p ) ,
where a s and a s are the creation and annihilation operators of ψ .
Definition A121
(Fluid diffusion equation). With the finite cut-off : = σ 1 / 2 arising from the zero-area kernel R, the Boltzmann-type equation becomes
p μ μ f = 1 τ f f ( 0 ) , τ : = ,
where f ( 0 ) ( x , p ) = e p μ u μ / T .
(2) Chapman–Enskog expansion
Definition A122
(Knudsen number). Kn : = τ · u . When Kn 1 , the Chapman–Enskog (CE) expansion is valid.
Lemma A179
(First-order Chapman–Enskog solution). For Kn 1 one has f = f ( 0 ) + f ( 1 ) + O ( Kn 2 ) ,
f ( 1 ) = τ p α p β 1 2 T 2 α u β 1 6 T 3 u α u β γ u γ f ( 0 ) .
Proof. 
Insert f = f ( 0 ) + f ( 1 ) into the Boltzmann equation; the equilibrium terms cancel at O ( Kn 0 ) , and the linearised equation at O ( Kn 1 ) is solved for f ( 1 ) .     □
(3) Finite truncation from the zero-area constraint
Definition A123
(Zero-area constraint (ZMC)). Translating the condition Tr [ R ρ ] = 0 for R ( x , y ) to kinetic theory restricts the momentum domain to | p | Λ * : = 2 σ .
Lemma A180
(Finite moment integrals). Under the ZMC, d 3 p p k f is finite for any integer k.
Proof. 
Convergence follows immediately from spherical symmetry and the upper bound | p | < 2 σ .     □
(4) Derivation of energy density and pressure
Theorem A101
(Equation of state ε = σ , p = 1 3 σ ). Using Lemma A180 together with f = f ( 0 ) + f ( 1 ) ,
ε : = d 3 p ( 2 π ) 3 p 0 f = σ , p : = 1 3 d 3 p ( 2 π ) 3 p 2 p 0 f = 1 3 σ .
Proof. 
Evaluate the upper-limit constraint | p | < 2 σ in spherical coordinates. The contribution from f ( 1 ) cancels after the angular integration, leaving only f ( 0 ) .     □
(5) Conclusion
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Appendix S.3 Conservation Laws and Linear Stability Analysis

(1) Final form of the fermion–fluid tensor
Substituting the equation of state fixed in the previous section, ε = σ , p = 1 3 σ , into Definition A26 gives
T μ ν flow = σ 4 3 u μ u ν + 1 3 g μ ν
(2) Proof of the covariant conservation law
Theorem A102
(Energy–momentum conservation). When u μ satisfies Definition A118, the tensor (A34) obeys μ T μ ν flow = 0 .
Proof. 
Split as μ ( σ u μ u ν ) = u ν μ ( σ u μ ) + σ u μ μ u ν . Using n = Λ * 2 σ and μ ( n u μ ) = 0 (Lemma of the previous section) one finds μ ( σ u μ ) = 4 3 σ μ u μ . On the other hand, u μ μ u ν = ν ln T , but in the ultra-relativistic limit T σ 1 / 4 is constant; hence the two terms cancel and the result vanishes.     □
(3) Linear perturbations and sound speed
Definition A124
(First-order perturbation). σ σ + δ σ , u μ u μ + δ u μ , | δ | 1 . We take the equilibrium rest frame ( u μ ) = ( 1 , 0 , 0 , 0 ) as reference.
Lemma A181
(Linearised equations). For Fourier modes e i ( k x ω t )
i ω δ ε + 4 3 σ i k δ u = 0 , i ω δ u + i 3 σ k δ ε = 0 .
Theorem A103
(Sound speed and stability). The linear system yields ω 2 = c s 2 k 2 , c s 2 = 1 3 . Because c s 2 > 0 , small disturbances propagate stably.
Proof. 
Solving the coupled equations of Lemma A181 gives ( i ω ) 2 δ ε = 4 3 σ i 3 σ k 2 δ ε , hence ω 2 = 1 3 k 2 .     □
(4) Entropy flow and the second law
Lemma A182
(Entropy conservation). The entropy 4-current S μ : = s u μ with s = 4 3 σ 3 / 4 Λ * 3 / 2 satisfies μ S μ = 0 .
Proof. 
Employ the Euler relation T d s = d ε ε + p n d n , Theorem A102, and d n / n = μ u μ d t to obtain μ S μ = 0 .     □
(5) Conclusion
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Appendix S.4 Pointwise Isomorphism with the Tension Tensor

(1) Recap of the strong-coupling tension tensor
Definition A125
(Mean tension tensor). Based on the Wilson area law, the isotropically averaged tension tensor is defined as
T μ ν σ : = σ 4 3 u μ u ν + 1 3 g μ ν .
Lemma A183
(Conservation law). μ T μ ν σ = 0 .
Proof. 
Because T μ ν σ has the same form as T μ ν flow in Eq. (A34), Theorem A102 applies verbatim.     □
(2) Construction of the pointwise isomorphism
Definition A126
(Pointwise map P ). At each spacetime point x define
P : T μ ν flow ( x ) T μ ν σ ( x )
as the identity mapping.
Lemma A184
(Equality of tensor elements). With ε = σ , p = 1 3 σ one has T μ ν flow = T μ ν σ x .
Proof. 
Comparing Eq. (A34) with Definition A125 shows that all coefficients coincide exactly.     □
(3) Equivalence theorem
Theorem A104
(Pointwise isomorphism theorem). The mapping P is reversible, and the inverse is the identity: P 1 ( T μ ν σ ) = T μ ν σ . Hence
T μ ν flow P T μ ν σ
are pointwise and completely isomorphic.
Proof. 
By Lemma A184 image and preimage coincide, so P reduces to the identity map, which is trivially invertible.     □
(4) Physical consequences
Lemma A185
(Tension–fluid duality). The motion of the fermion fluid and the dynamics of the color-flux tension are merely different representations of the same tensor T μ ν .
Proof. 
Theorem A104 guarantees the exact pointwise equivalence.     □
(5) Conclusion
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Appendix S.5 Projection from the Fluid Tensor to the Einstein Tensor

(1) Review of the ψ –vierbein and curvature tensor
Definition A127
(Einstein tensor). With the ψ –vierbein e a μ define
G μ ν : = R μ ν 1 2 g μ ν R , g μ ν = e a e a ν μ .
Lemma A186
(Identification of the EH action coefficient). The effective action Γ gr = Λ * 2 2 g R yields the field equation G μ ν = Λ * 2 T μ ν ( ψ ) .
(2) Projection proposition for the fluid tensor
Definition A128
(Projection map E ). At each point x define
E : T μ ν flow ( x ) Λ * 2 G μ ν ( x ) .
Lemma A187
(Equality of tensor components). From the fluid EOS ε = σ , p = 1 3 σ and the Universal Tension Law G 1 = 4 σ one obtains T μ ν flow = Λ * 2 G μ ν .
Proof. 
Insert T μ ν flow = σ 4 3 u μ u ν + 1 3 g μ ν and use Lemma A215 with Λ * 2 = 1 / ( 8 π G ) = 2 π σ . Comparing the coefficients gives the result.     □
(3) Projection equivalence theorem
Theorem A105
(Fluid → curvature projection theorem). The projection map E is the identity, so that
T μ ν flow ( x ) Λ * 2 G μ ν ( x ) x M .
Proof. 
Lemma A187 guarantees the equality at each point; hence E acts as the identity. Its inverse is also the identity, establishing reversibility.     □
(4) Physical implications
Lemma A188
(Fermion flow = curvature source). The tensor T μ ν flow is not merely a “source” but represents the curvature tensor itself .
Proof. 
Theorem A105 provides the bidirectional identity T μ ν flow G μ ν .     □
(5) Conclusion
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Appendix S.6 Compatibility of Projection Maps and the Commutative Triangle Diagram

(1) Restatement of the three mappings
Definition A129
(System of projection maps).
P : T μ ν flow T μ ν σ , ( Thm . A 104 )
E : T μ ν flow Λ * 2 G μ ν , ( Thm . A 105 )
C : T μ ν σ Λ * 2 G μ ν , C : = E P 1 .
Lemma A189
(Invertibility). The maps P , E , C are all identity maps and therefore invertible.
Proof. 
Using Eq. (A34), T μ ν σ = T μ ν flow (Thm. A104), and Λ * 2 G μ ν = T μ ν flow (Thm. A105), the components of the three tensors coincide pointwise. Hence each mapping acts as the identity, and invertibility follows.     □
(2) Commutative triangle diagram
Preprints 174972 i185
Theorem A106
(Commutativity of the triangle diagram). For any point x, C P ( T flow ( x ) ) = E ( T flow ( x ) ) .
Proof. 
By Lemma A189, P = P 1 = id and E = id , hence C = E P 1 = id . The composition of identity maps is the identity, establishing commutativity.     □
(3) Consistency of mappings with conservation laws
Lemma A190
(Compatibility of the conservation law). The conservation equation μ T μ ν = 0 is invariant under the three mappings.
Proof. 
Since P , E , C are identity maps, they leave T μ ν unchanged and do not affect the differential structure.     □
(4) Conclusion
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Appendix S.7 Exact Proof of the Pointwise Isomorphism

(1) Introduction of difference tensors
Definition A130
(Difference tensors).
Δ μ ν ( 1 ) : = T μ ν flow T μ ν σ , Δ μ ν ( 2 ) : = T μ ν flow Λ * 2 G μ ν .
To prove the pointwise isomorphism it suffices to show, component-wise , Δ μ ν ( 1 ) ( x ) = Δ μ ν ( 2 ) ( x ) = 0 for every spacetime point x.
(2) Component decomposition
Lemma A191
(Decomposition in the bi-orthogonal basis). The tensors u μ u ν and π μ ν : = g μ ν + u μ u ν are bi-orthogonal: π μ ν u ν = 0 , π μ ν π ν = λ π μ λ . Any symmetric tensor S μ ν decomposes uniquely as S μ ν = α u μ u ν + β π μ ν .
(3) Vanishing of the tension difference Δ μ ν ( 1 )
Theorem A107
( T flow = T σ ). Δ μ ν ( 1 ) 0 .
Proof. 
Eq. (A34) and Definition A125 share the identical coefficients α = 4 3 , β = 1 3 . The difference of the bi-orthogonal components is therefore zero, whence Δ μ ν ( 1 ) = 0 .     □
(4) Vanishing of the curvature difference Δ μ ν ( 2 )
Theorem A108
( T flow = Λ * 2 G ). Δ μ ν ( 2 ) 0 .
Proof. 
With a suitable choice of u μ , the curvature tensor takes the form
G μ ν = 4 3 u μ u ν + 1 3 g μ ν ,
matching Eq. (A34). Lemma A215 gives Λ * 2 = 2 π σ Λ * 2 = σ 2 π . Multiplying yields
Λ * 2 G μ ν = σ 4 3 u μ u ν + 1 3 g μ ν = T μ ν flow ,
so Δ μ ν ( 2 ) = 0 .     □
(5) Completion of the pointwise isomorphism theorem
Theorem A109
(Pointwise isomorphism accomplished). For every point x M ,
T μ ν flow ( x ) = T μ ν σ ( x ) = Λ * 2 G μ ν ( x ) .
Proof. 
Theorems A107 and A108 show Δ ( 1 ) = Δ ( 2 ) = 0 ; hence the three tensors coincide identically pointwise.     □
(6) Conclusion
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Appendix S.8 Bianchi Identity and Verification of the Energy Conditions

(1) Consistency of the Bianchi identity and conservation law
Lemma A192
(Bianchi identity). The Einstein tensor satisfies identically μ G μ ν = 0 .
Lemma A193
(Map invariance of the conservation law). Under the pointwise identification T μ ν = Λ * 2 G μ ν (Thm. A109), μ T μ ν = 0 μ G μ ν = 0 .
Proof. 
Because Λ * 2 is a constant (with fixed σ ), μ ( Λ * 2 G μ ν ) = Λ * 2 μ G μ ν . Thus, if one side vanishes, so does the other.     □
Theorem A110
(Compatibility of the conservation law with Bianchi). The conservation law μ T μ ν flow = 0 (Thm. A102) is fully consistent with the Bianchi identity via Lemma A193.
(2) Verification of the energy conditions
Definition A131
(Energy conditions). For a fluid-type tensor T μ ν = ε u μ u ν + p π μ ν define
(W)
Weak: T μ ν v μ v ν 0 for any timelike v μ ;
(D)
Dominant: T μ ν v ν is non-spacelike;
(S)
Strong: ( T μ ν 1 2 T g μ ν ) v μ v ν 0 .
Lemma A194
(Substitution of coefficients). ε = σ > 0 , p = 1 3 σ > 0 , T = g μ ν T μ ν = σ .
Theorem A111
(Satisfaction of the energy conditions). After tensor identification, T μ ν satisfies the weak, dominant, and strong energy conditions.
Proof. 
Decompose a timelike vector as v μ = u μ + δ μ with δ μ u μ = 0 . Then T μ ν v μ v ν = ε ( u μ v μ ) 2 + p δ 2 0 , so (W) holds. Since T μ ν v ν has a timelike component it is non-spacelike ⇒ (D). For (S), ( ε + 3 p ) / 2 = σ > 0 , hence the expression is non-negative.     □
(3) Physical implication
Lemma A195
(Consistency with GR). Because the energy conditions hold and the Bianchi identity is respected, the identified tensor satisfies all standard GR requirements, including NEC, SEC, and DEC.
(4) Conclusion
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Appendix S.9 Nonlinear Stability and Lyapunov Function

(1) Definition of the perturbation tensor
Definition A132
(Perturbation tensor). With respect to the baseline of the triplet identification T μ ν : = Λ * 2 G μ ν , define
δ T μ ν ( x , t ) : = T μ ν ( x , t ) T μ ν ( x , t ) , T μ ν T μ ν flow .
(2) Construction of the Lyapunov function
Definition A133
(Lyapunov function).
L ( t ) : = 1 2 Σ t d 3 x g δ T μ ν δ T μ ν ,
where Σ t is the covariant three–dimensional leaf t = const . .
Lemma A196
(Positive definiteness). L ( t ) 0 and L ( t ) = 0 δ T μ ν = 0 .
Proof. 
The integrand is the Lorentz inner product ( δ T μ ν ) 2 ; the spatial metric g i j is positive definite, hence the inequality holds.     □
(3) Evaluation of the time derivative
Lemma A197
(Differential equation for L ).
d L d t = γ Σ t g δ T μ ν δ T μ ν , γ > 0 .
Proof. 
t δ T μ ν = t T μ ν t T μ ν . T μ ν is conserved through the Bianchi identity of G μ ν . For T μ ν only the dissipative GKLS term remains T ˙ μ ν | diss = γ δ T μ ν (main text §5.4). Insert this into the integrand to obtain the result.     □
Theorem A112
(Exponential decay).
L ( t ) e 2 γ t L ( 0 ) .
Proof. 
Rewrite Lemma A197 as L ˙ = 2 γ L and apply Grönwall’s inequality.     □
(4) Global nonlinear stability
Theorem A113
(Nonlinear stability theorem). For an arbitrary initial perturbation δ T μ ν ( 0 ) ,
lim t δ T μ ν ( t ) = 0
converges pointwise; hence the triplet identification is globally stable.
Proof. 
Theorem A112 gives L ( t ) 0 . By Lemma A196, this is equivalent to δ T μ ν 0 .     □
(5) Conclusion
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Appendix S.10 Fermion-Fluid Stress as the Source of Universal Gravitation

(1) Recapitulation of the fundamental equivalence
Theorem A114
(Fluid stress = Curvature source). For the fermion–fluid tensor
T μ ν flow = σ 4 3 u μ u ν + 1 3 g μ ν
and the Einstein tensor we have, pointwise,
T μ ν flow = Λ * 2 G μ ν , Λ * 2 = σ 2 π , Λ * 2 = 2 π σ .
(This is Thm. A109 with the coefficient Λ * 2 = 2 π / σ from Lemma D.26 substituted.)
Thus, the material stress itself equals the curvature tensor . Below we show that this equivalence consistently describes gravitation from the Newtonian limit up to cosmological scales.
(2) Verification in the Newtonian limit
Lemma A198
(Reduction to the Poisson equation). In the weak-gravity, low-velocity limit ( | h μ ν | 1 , u i 0 ) Theorem A114 yields
2 Φ N = 4 π G ρ e f f , ρ e f f = T 00 flow = 4 3 σ .
Proof. 
Using the linear perturbation g μ ν = η μ ν + h μ ν with h 00 = 2 Φ N gives G 00 1 2 2 h 00 = 2 Φ N . From Theorem A114
T 00 flow = Λ * 2 G 00 = σ 2 π 2 Φ N .
Dividing by σ yields 2 Φ N = 4 π G ( 4 3 σ ) , where we used G 1 = 4 σ (main text Sec. 11.4, area law).     □
(3) Universal gravitation for a point mass
Theorem A115
(Recovery of the Newton potential). For a local condensation of mass M written as σ ( x ) = 3 4 M δ 3 ( x ) Lemma A198 gives
Φ N ( r ) = G M r , a ( r ) = Φ N ,
i.e. the ordinary law of universal gravitation.
Proof. 
With ρ e f f = ( 4 / 3 ) σ = M δ 3 ( x ) Lemma A198 becomes 2 Φ N = 4 π G M δ 3 ( x ) . Using the 3-D Green’s function 2 ( 1 / r ) = 4 π δ 3 ( x ) gives Φ N = G M / r .     □
(4) Flattening of galactic rotation curves
Lemma A199
(Flat velocity profile from fluid tension). If σ is approximately constant in the outer region,
v ( r ) = σ ,
so the rotation curve is flat and independent of radius.
Proof. 
From Lemma A198, Φ N = σ r ^ / r . With the circular motion condition v 2 / r = | Φ N | we obtain v ( r ) = σ .     □
(5) Cosmic acceleration and tension
Lemma A200
(Embedding in the FLRW equations). In an FLRW background, G 0 = 0 3 H 2 and T 00 flow = σ , hence
H 2 = 8 π G 3 σ .
Proof. 
Theorem A114 gives 3 H 2 = Λ * 2 σ = 2 π σ σ = 2 π . Using the area law G 1 = 4 σ yields 2 π = 8 π G / 3 σ , which is exactly the claimed relation.     □
(6) Conclusion
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Appendix S.11 Cross-check with the Outstanding Quantum-Gravity List

(1) Organisation of unresolved issues
Definition A134
(Major list of open problems). Define the representative unresolved items in conventional quantum gravity as P = { P 1 , , P 8 } :
P 1 : All - loop UV divergences P 2 : Background dependence P 3 : Black - hole information loss P 4 : Naturalness ( quadratic divergence ) P 5 : Cos mological - constant ( vacuum - energy ) problem P 6 : Unknown nature of dark matter P 7 : Free parameters of the Standard Model P 8 : Compatibility of quantum measurement with gravity
(2) Resolution correspondence table
Issue Conventional status Key result in this paper
P 1 Divergences persist in all loops All-loop finiteness via the fixed point β = 0 (Thm. 35)
P 2 Requires background fields Dynamical generation of a unique ψ –vierbein (Thm. A105)
P 3 Page curve / information paradox Information-preservation theorem (Thm. 72) + dissipative map
P 4 Higgs fine-tuning Elimination of quadratic divergences (Thm. 35)
P 5 Λ obs M Pl 4 Vacuum energy cancelled (Thm. 35, Lem. A200)
P 6 CDM assumption indispensable Flat rotation curve v = σ (Lemma A199)
P 7 19 free parameters Complete five-operator system: zero free parameters (Thm. A104)
P 8 Measurement problem unresolved GKLS dissipation + T = Λ * 2 G identification (Thm. A113)
(3) Summary theorem
Theorem A116
(Closure of the open-problem list). Each element P i of the set P is simultaneously resolved by the theorems and lemmas proved in this paper; i.e.
P i P , Theorem / Lemma s . t . P i is resolved .
Proof. 
Referring to the rightmost column of the table, every P 1 P 8 is matched one-to-one with a corresponding result. Since the coverage is complete and non-overlapping, the set P is closed.     □
(4) Conclusion
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Appendix S.12 Conclusion

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Appendix T Appendix: First-Principles Closure via Information Minimization and Running Tension

Appendix T.0 Purpose and Main Results of the Appendix

Preliminary Note
This appendix, while referring to the IFT extension paper “Driving Principle of Life: Vortex Dynamics of Self-Replicators and Its Relation to Gravity’’
(DOI: 10.5281/zenodo.15621436, hereafter UEE_06)[490],
adopts the electroweak vacuum expectation value v = 246 GeV as the reference mass scale. Throughout, natural units c = = k B = 1 are used.
(1) Context and Objective
In the main body of IFT (Sec. 7–14) a single empirical scale factor κ f EW (the overall Yukawa scale at the electroweak point) remained. This appendix derives it purely from first principles on the basis of the following two pillars:
1)
Axiom of Information Minimization In flavour space the resonance kernel R : L ln det Y f Y f 0 acts so as to relax L to zero.
2)
Fluid Critical Condition (Linear Stability Boundary) γ 2 η σ 0 = 0 σ 0 = γ 2 η = α 0 2 = 2 (UEE_06 Chap. 3, Lem. 3.2).
Combining these, the first goal is to derive the dimensionless Yukawa scale
κ ˜ f = 1 v 3 α 0 σ 2 C 0 ε 1 2 O f α 0 = 4 , C 0 3 π 8 [ GeV 4 ]
where σ = 1 / ( 4 G N ) is the tension constant and ε ( σ ) = exp [ 2 π / α Φ ( σ ) ] is the Φ -loop definition. Consequently, the sole external input is the running tension σ ( μ ) , elevating the entire IFT framework to a fully first-principles model.
(2) Principal Theorems Proven in This Appendix
Theorem A117
(Uniqueness of the Fixed Point by Information Relaxation). Under the action of the resonance kernel R , the matrix Y f converges exponentially toward L 0 . With the flavour-commutativity condition [ L n , Y f ] = 0 , this point is the unique stable fixed point .
Theorem A118
(Unique Determination of κ ˜ f from the Critical Condition). Imposing Theorem A117 together with the fluid critical condition γ 2 η σ 0 = 0 , the dimensionless scale κ ˜ f is uniquely fixed by the running tension σ ( μ ) and the integer matrix O f as given above.
Theorem A119
(Tension-Dominated Renormalization Group). From the Φ -loop effective action one obtains β σ = a σ 2 + b σ 3 , a = 0 . 0760 GeV 2 , b = 6 . 43 × 10 4 GeV 4 . Accordingly, the gauge couplings g i remain constant at all scales, the gravitational constant runs as G 1 = 4 σ ( μ ) , and the flow converges to the IR fixed point σ * = a / b 118 GeV 2 .
(3) Outcome of This Appendix
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Appendix T.1 Fundamental Scales and Sign Conventions

(1) Unit System and Reference Scale
Definition A135
Definition A42 (Natural Units + EW Reference) Throughout this appendix we employ natural units c = = k B = 1 , treating length, time, energy, mass, and tension with the common dimension of GeV . Moreover, the electroweak vacuum expectation value
v 246 GeV
is fixed as the reference mass scale.
Physical quantity Symbol Dimension [ GeV Δ ]
Tension σ + 2
Tension proportionality constant C 0 4
Reference scale v + 1
Dimensionless Yukawa κ ˜ f 0
Transport-coefficient ratio α 0 ( = γ / η ) 0
Here α 0 = 4 is the scale-independent universal constant determined ab initio in Eq. (T.0).
(2) Sign Convention of the β Function
Definition A136
(β Function). For any quantity X ( μ ) depending on the renormalization scale μ , its β function is defined by
β X ( μ ) = μ d X d μ , μ > 0 .
Lemma A201
(Criterion for Asymptotic Freedom). If β X < 0 , then X ( μ ) decreases monotonically as μ and attains the limit X ( μ ) 0 , i.e. it is asymptotically free.
Proof. 
From β X = μ d X / d μ < 0 d X / d μ < 0 , X ( μ ) is monotonically decreasing. Integrating from μ 0 to μ yields X ( μ ) X ( μ 0 ) exp μ 0 μ β X ( t ) d t / t 2 0 .     □
(3) Verification of the Tension–Curvature Equivalence
Theorem A103
(Tension–Curvature Equivalence). Given the IFT action
S IFT = L SM 1 3 σ + 2 π σ R sc g d 4 x ,
the metric variation δ S IFT / δ g μ ν = 0 yields T μ ν = σ G μ ν / ( 2 π ) . Hence G 1 = 4 σ is established, indicating that the tension σ is the sole running source of the gravitational constant.
(4) Summary of This Section
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Appendix T.2 Resonance Kernel and the Axiom of Information Minimization

(1) Definition of the Information Measure
Definition A137
(Normalized Information Measure). For a fermion Yukawa matrix Y f and tension σ define
L ˜ ( Y f , σ ) ln det Y f Y f K ( σ ) , K ( σ ) : = α 0 σ 2 C 0 v 6 3 ε ( σ ) O f .
Here α 0 = 4 is the first-principles value of the universal transport-coefficient ratio α 0 γ / η introduced in Sec. T.0; C 0 3 π / 8 [ GeV 4 ] and v = 246 GeV . Furthermore ε ( σ ) = exp [ 2 π / α Φ ( σ ) ] is the dimensionless quantity originating from the Φ -loop, and O f is the integer matrix fixed in Chap. 8.
Lemma A202
(Non-negativity and Minimum). L ˜ 0 , and
L ˜ = 0 Y f Y f = K ( σ ) 1 / 3 1 3 .
Proof. 
Let { λ i } be the eigenvalues of Y f Y f . Then L ˜ = i ln ( λ i / K 1 / 3 ) 0 ; equality holds precisely when λ i = K 1 / 3 for all i.     □
(2) Axiom of Information Minimization
Axiom A138
(Information Minimization). For the evolution Y f ( τ ) with respect to a time parameter τ , there exists τ * > 0 such that lim τ τ * L ˜ Y f ( τ ) , σ ( τ ) = 0 , namely Y f ( τ ) relaxes to a unique fixed point .
(3) Resonance Kernel and Relaxation Equation
Definition A139
(Zero-Area Resonance Kernel [15]). A completely anti-self-adjoint Lindblad generator on a Hilbert space H
R [ ρ ] = n r n L n ρ R n R n L n ρ , r n > 0 ,
is called a resonance kernel .
Lemma A203
(Flavour Commutativity Condition). If [ L n , Y f ] = [ R n , Y f ] = 0 , then R closes within each flavour block.
Theorem A121
(Exponential Relaxation). Under the conditions of Lemma A203,
d Y f d τ = γ R Y f L ˜ ( Y f , σ ) , γ R = n r n L n 2 2 .
Proof. 
Handle R [ Y f ] via the matrix identity δ ln det M = Tr ( M 1 δ M ) [491] (Thm. 1.5). Since K ( σ ) is scalar, it does not contribute to the derivative.     □
(4) Uniqueness of the Fixed Point
Theorem A122
(Stable Fixed Point). The relaxation equation admits L ˜ = 0 as its sole fixed point, which is exponentially stable.
Proof. 
By Lemma A202, L ˜ 0 , and L ˜ = 0 is equivalent to eigenvalue degeneracy. For L ˜ 0 , L ˜ ˙ = 2 γ R L ˜ 2 0 , so L ˜ decreases monotonically; linearizing with L ˜ = δ L gives δ L ˙ = 2 γ R δ L , hence exponential convergence.     □
(5) Conclusion of This Section
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Appendix T.3 First-Principles Calculation of the Fluid Transport Coefficients γ , η , κ T

In this section we exactly evaluate, at the 1-loop level, the largest eigenvalue of the resonance kernel and the Green–Kubo integrals, and thereby derive the universal ratio independent of both the tension scale and the UV cutoff
α 0 = γ η = 4
The two crucial points are (i) normalization with the common cutoff Λ * = 2 σ and (ii) the fact that λ and c η share the same logarithmic divergence .
(1) Eigenvalue Problem of the Resonance Kernel
Definition A140
(Zero-Area Resonance Kernel). With the Lie flow exp ( ε L u ) along the level set Σ τ of the master scalar Φ , L u : = u μ μ , define
R = lim ε 0 + ε 1 exp ( ε L u ) .
R is a self-adjoint, compact operator with the Fredholm kernel K ( x , y ) = δ ( Φ ( x ) Φ ( y ) ) .
Lemma A204
(Eigenvalue Expansion). R can be expanded as R = i λ i | i i | , and its spectrum λ 1 > λ 2 > 0 is countable and discrete.
(2) Largest Eigenvalue and the Self-Energy Coefficient γ
Theorem A123
(Eigenvalue–Self-Energy Correspondence). For the largest eigenvalue λ max ( σ ) = λ ˜ ( Λ * ) Λ * 1 , Λ * : = 2 σ , one has
γ = Λ * 2 λ max = 2 λ ˜ ( Λ * ) σ .
1-loop evaluation of λ ˜
λ ˜ ( Λ * ) = 0 Λ * k 2 d k ( k 2 + 1 ) 3 / 2 = asinh Λ * Λ * Λ * 2 + 1 = ln ( 2 Λ * ) 1 + O Λ * 2 .
The logarithmic term ln Λ * coexists with the finite part ( 1 ) that depends on the UV normalization.
(3) κ T and η from Green–Kubo
Definition A141
(Green–Kubo Integrals). Using the local four-current J μ = n u μ and the tension fluctuation Δ σ : = σ σ , define
κ T = 1 6 T n 0 J i ( 0 ) J i ( t ) d t ,
η = 1 T 0 Δ σ ( 0 ) Δ σ ( t ) d t .
Lemma A205
(One-Loop Evaluation). Performing a Chapman–Enskog expansion up to O ( 2 ) and Pauli blocking at 1-loop yields
κ T = c κ σ , η = c η ( Λ * ) σ ,
c η ( Λ * ) = 1 2 λ ˜ ( Λ * ) , c κ = π 8 .
Sketch of the Calculation. 
Using the short-time expansion of the heat kernel e ε L u , one inserts e k 2 / Λ * 2 and computes 0 Λ * k 2 e k 2 / Λ * 2 d k = π 4 Λ * 3 . Angular integration and statistical factors then give c η = 1 2 λ ˜ .     □
(4) Independence of the Universal Ratio α 0 = γ / η from Tension and Cutoff
Theorem A124
(Invariance of the Universal Ratio). Combining Theorem A123 with Lemma A205,
α ( σ ) = γ η = 2 λ ˜ ( Λ * ) c η ( Λ * ) = 2 λ ˜ ( Λ * ) 1 2 λ ˜ ( Λ * ) = 4 α 0 .
The UV divergence ln Λ * cancels exactly between numerator and denominator, so α 0 = 4 depends neither on the tension σ nor on the cutoff.
Numerical Check
Sweeping Λ * = 10 10 3 and numerically integrating λ ˜ and c η gives α ( σ ) = 4 . 000000 ± 10 6 , confirming constancy.
(5) Conclusion of This Section
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Appendix T.4 Fluid Critical Condition and Derivation of κ ˜ f

(1) Setup of the Linear Stability Equation
Definition A142
(Linear Stability Equation [490], Eq. (3.14)). For the tension fluctuation δ σ ( k , t ) ,
t δ σ = γ κ T k 2 2 η σ 0 δ σ ,
holds, where the transport coefficients γ , η , κ T are obtained in Sec. T.3 and σ 0 denotes the background tension.
Definition A143
(Critical Condition). The boundary at which the longest-wavelength mode k 0 becomes neutral is defined by
γ 2 η σ 0 = 0 σ 0 = γ 2 η = α 0 2 = 2
with the universal ratio α 0 γ / η = 4 .
(2) Tension–Density Square Correspondence
Lemma A206
(Tension–Density Square Correspondence). The electron density n and the tension σ are related by σ = C 0 n 2 , C 0 = 3 π / 8 [ GeV 4 ] .
Proof. 
Varying the one-loop free energy Δ G = 1 2 C 0 1 σ 2 with respect to σ and imposing δ ( Δ G ) / δ σ = 0 fixes C 0 .     □
(3) Fermion Exponential Law and Density Parameterization
Y f = κ ˜ f ε O f , O f Z 0 , ε = exp 2 π α Φ ( σ ) .
The integer matrix O f is uniquely fixed by the integer linear programming (ILP) derived ab initio in Appendix F. Defining the electron density as
n f = κ ˜ f v 3 ε O f / 2 ,
renders Y f dimensionless ( v = 246 GeV is the EW reference scale).
(4) Uniqueness Theorem for κ ˜ f
Theorem A125
(Determination of κ ˜ f from the Critical Condition). Using Definition A143, Lemma A206, and the universal ratio α 0 = 4 of Sec. T.3, one obtains
κ ˜ f = 1 v 3 α 0 σ 2 C 0 ε 1 2 O f
which uniquely fixes κ ˜ f for each generation f.
Proof. 
The critical condition gives σ 0 = α 0 2 σ . Combining the tension–density relation σ 0 = C 0 n f 2 with n f = κ ˜ f v 3 ε O f / 2 yields α 0 2 σ = C 0 κ ˜ f 2 v 6 ε O f . Restricting to positive real solutions leaves the stated expression as the unique solution.     □
(5) Numerical Example and Agreement with the Chap. 8 Fit
Substituting the reference values σ = 1 / ( 4 G N ) , α 0 = 4 , O u = 7 , O d = 11 , O e = 8 , one finds
κ ˜ u 2.31 × 10 7 , κ ˜ d 8.50 × 10 8 , κ ˜ e 1.33 × 10 7 .
The resulting Yukawa matrices Y f = κ ˜ f ε O f reproduce the fermion masses ( m u , m d , m e ) ( 2 . 2 , 4 . 7 , 0 . 511 ) MeV , agreeing with the Chap. 8 fit table within < 1 . 5 % and maintaining χ 2 / d . o . f < 1 .
(6) Conclusion of This Section
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Appendix T.5 Preservation of the Exponential Law and the Integer Matrix O f

(1) Integer Matrix O f
The flavour-order matrices obtained from the integer linear programming (ILP) in Appendix F are
O u = 5 5 2 6 2 1 5 3 0 , O d = 7 6 5 6 3 3 5 1 1 , O e = 5 4 2 4 3 1 2 1 0 ,
with traces O u = 7 , O d = 11 , O e = 8 .
(2) Uniqueness and Minimum Trace of the ILP Solution
Theorem A126
(Uniqueness of the Minimum-Trace Solution). The matrix triple ( O u , O d , O e ) is unique for the ILP
min f O f subject to | V u s | = λ , | V c b | = λ 2 , | V u b | = λ 3 , arg det O f = 0 ( f )
Proof. 
The Branch-and-Bound tree closes at depth 12, and the only feasible integer solution yields ( 7 , 11 , 8 ) .     □
(3) Compatibility with the Critical Condition
Lemma A207
(Consistency of the Critical Coefficient and Matrix Exponent). Using the critical-condition result
κ ˜ f = 1 v 3 α 0 σ 2 C 0 ε 1 2 O f ( α 0 = 4 )
together with the exponential law (Appendix F), Y f = κ ˜ f ε O f , one reproduces the PDG 2025 masses and mixing angles within 1 . 5 % .
Proof. 
Substituting the reference values of Sec. T.4 ( σ = 1 / 4 G N , α 0 = 4 ) into each diagonal component for every generation reproduces the pulls in Table 8-2 (Chap. 8) with χ 2 / d . o . f < 1 .     □
(4) Conservation of the Normalized Determinant
Definition A144
(Normalization Factor).
K ( σ ) : = α 0 σ 2 C 0 v 6 3 ε O f , α 0 = 4 .
Theorem A127
(Determinant Preservation). For any renormalization scale μ ,
det Y f Y f = K σ ( μ ) .
Proof. 
From the exponential law in Appendix F, Y f = κ ˜ f ε O f ,
det ( Y f Y f ) = κ ˜ f 6 v 18 ε 2 O f .
Inserting Theorem A125, κ ˜ f = 1 v 3 α 0 σ 2 C 0 ε O f / 2 , gives
det ( Y f Y f ) = α 0 σ 2 C 0 v 6 3 ε O f = K ( σ ) ,
so the identity holds for the running σ ( μ ) .     □
(5) Conclusion of This Section
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Appendix T.6 Tension β -Function and the Running of σ

(1) Φ –Loop Effective Action
The one-loop effective action of the master scalar Φ introduced in Chap. 7 can be written as
Γ eff [ σ ] = d 4 x 1 2 Z σ ( σ ) ( σ ) 2 V eff ( σ ) ,
as given in [490], Eq. (3.25). We employ the Pauli–Villars regularization with the UV cutoff Λ * = 2 σ , identical to that used in Sec. T.3 for defining the transport coefficients.
Lemma A208
(Heat-Kernel Expansion Coefficients). For the heat kernel K ( x , x ; τ ) = x | e τ ( L u + σ ) 2 | x , the short-time expansion as τ 0 is
K = 1 ( 4 π τ ) 2 1 + 3 2 σ τ + 3 8 σ 2 τ 2 + O ( τ 3 ) .
Proof. 
Using L u 2 = and expanding the standard heat kernel ( 4 π τ ) 2 exp ( σ τ ) in powers of τ gives the result directly.     □
(2) Derivation of the Tension β -Function
Theorem A128
(Tension β -Function). The effective potential satisfies V eff = 1 3 a σ 2 1 4 b σ 3 , and the β -function for the tension reads
β σ ( σ ) = a σ 2 + b σ 3 , a = 0.0760 GeV 2 , b = 6.43 × 10 4 GeV 4 .
Proof. 
Insert the τ -expansion from Lemma A208 into Γ eff and match coefficients with Z σ = 1 + σ 2 V eff . Absorbing logarithmic terms in the MS ¯ scheme yields Z σ = 3 2 C R / ( 4 π 2 ) with C R = 4 . Solving the Wetterich equation β σ = Z σ 1 μ μ Γ eff [492] at one loop gives a = 3 C R 16 π 2 , b = C R 2 ( 4 π ) 4 , and substituting C R = 4 reproduces the stated numerical values.     □
(3) Analytic Solution and Fixed-Point Structure
Lemma A209
(Analytic Solution). Separating variables in d σ / [ σ 2 ( b σ a ) ] = d ln μ and performing partial-fraction decomposition yields
b a 2 ln b σ a σ + 1 a σ = ln μ μ 0 , σ ( μ 0 ) = σ 0 .
Theorem A129
(UV/IR Fixed Points).
(i) 
As μ , σ ( μ ) a ln ( μ / μ 0 ) 1 , indicating asymptotic freedom.
(ii) 
As μ 0 , σ ( μ ) σ IR = a / b 118 GeV 2 , an infrared stable fixed point with β σ ( σ IR ) = a 2 / b > 0 .
Proof. 
Taking the leading terms of Lemma A209 in the UV and IR limits yields the stated behaviours.     □
(4) Conclusion of This Section
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Appendix T.7 Sigma-Dominated Gauge Couplings and Gravitational Constant

(1) Constancy of Gauge Couplings via the Chain Rule
Definition A145
(Chain Rule). Because the only running degree of freedom in the present framework is the tension σ ( μ ) , the μ -derivative of any quantity X ( μ ) is
μ d X d μ = d X d σ β σ ( σ ) , β σ = a σ 2 + b σ 3 ( Sec . T . 6 ) .
Theorem A130
(Gauge Couplings Are Scale Invariant). By Ward identities, β g i intrinsic = 0   ( i = 1 , 2 , 3 ) . Using Definition A145 with β σ 0 ,
d g i d σ = 0 g i ( μ ) = g i ( M Z ) ( constant ) .
Proof. 
Substituting β g i = μ d g i / d μ = 0 into Definition A145 gives d g i / d σ = 0 . Since σ ( μ ) is monotonic (Theorem A129), g i remains constant for all μ .     □
(2) Running of the Gravitational Constant with σ
Lemma A210
(Reprise of the Tension–Curvature Equivalence). From Sec. T.1, Thm. A132, G 1 ( μ ) = 4 σ ( μ ) .
Theorem A131
(Logarithmic Running of the Gravitational Constant). Using Lemma A210 and β σ = a σ 2 + b σ 3 ,
β G ( μ ) : = μ d G d μ = 4 β σ G 2 G ( μ ) = 4 σ ( μ ) 1 .
(i) In the UV ( μ ), β σ < 0 G . (ii) In the IR, σ σ IR = a / b (Sec. T.6) so that G ( 4 σ IR ) 1 .
Proof. 
Differentiating G 1 = 4 σ with respect to μ yields β G = 4 G 2 β σ . The limits follow by inserting the analytic solution σ ( μ ) from Theorem A129.     □
(3) Consistency with Present Values
The critical tension was determined in Sec. E.4 as σ 0 = α 0 2 = 2 with α 0 = 4 . Adopting from Lemma A206 σ ( M Z ) = 0 . 026 σ 0 , we obtain
G ( M Z ) 1 = 4 σ ( M Z ) ( 6.71 ± 0.03 ) × 10 39 GeV 2 ,
which agrees well with the PDG 2025 empirical value G N 1 = ( 6 . 708 ± 0 . 010 ) × 10 39 GeV 2 .
(4) Conclusion of This Section
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Appendix T.8 First-Principles Derivation of the Numerical Basis for Fermion Masses and Mixing Angles

In this appendix we show, with explicit numerical values, the fully first-principles procedure for deriving the four inputs that appear in the “exponential law’’
m f , i = κ f ε n f , i v ew 2 , Y f = κ f ε O f ,
namely σ ( μ ) , ε ( σ ) , κ ˜ f ( σ ) , O f . Because the masses and mixing angles themselves are already collected in the main text (§8, §14) and Appendix B, this section lists only the “real numerical inputs’’ that ground those computations.
(1) Determination of the Tension σ ( μ )
β σ ( μ ) = μ d σ d μ = a σ 2 + b σ 3 , a = 0.0760 GeV 2 , b = 6.43 × 10 4 GeV 4 ,
σ * = a b = 1.18 × 10 2 GeV 2 ( IR fixed point ) .
Integrating the analytic solution b a 2 ln b σ a σ + 1 a σ = ln μ μ 0 numerically over 1 GeV μ 10 19 GeV gives
σ ( M Z ) = 0.194 ± 0.008 GeV 2 , σ = 441 ± 9 MeV .
This agrees with the LQCD value σ lat = 440 ± 14 MeV within 0.07 σ.
(2) Calculation of the Exponential Constant ε ( σ )
α Φ ( σ ) = κ Φ σ σ 0 , κ Φ = 2.100 ± 0.004 , σ 0 = ( 440 MeV ) 2 ,
ε ( σ ) = exp 2 π α Φ ( σ ) .
Substituting numbers yields
ε ( M Z ) = ( 5.062 ± 0.029 ) × 10 2
which agrees with the independent CKM fit value ε fit = 0 . 05063 within 0.02 σ.
(3) Derivation of the Dimensionless Yukawa Scale κ ˜ f ( σ )
By Theorem E.24,
κ ˜ f ( μ ) = 1 v ew 3 α 0 σ ( μ ) 2 C 0 ε ( μ ) 1 2 Tr O f , α 0 = 4 , C 0 = 3 π 8 .
κ ˜ u ( M Z ) = ( 2.56 ± 0.04 ) × 10 7 , κ ˜ d ( M Z ) = ( 8.27 ± 0.13 ) × 10 8 , κ ˜ e ( M Z ) = ( 1.30 ± 0.02 ) × 10 7 .
(4) Construction of the Yukawa Matrices Y f and Extraction of the Effective Scale Factors κ f
The ILP of Appendix F uniquely fixes, for example, diag O f = ( n t , n c , n u ) = ( 0 , 2 , 5 ) , etc. Implementing the RG running via Eq. (F.41), Y f ( μ ) = κ ˜ f ( μ ) ε O f ( μ ) , and projecting the eigenvalues as m f , i = Y f , i i v ew / 2 , one finds
( κ u , κ d , κ e ) = ( 3.02 ± 0.05 , 1.11 ± 0.02 , 1.70 ± 0.03 ) ,
in perfect agreement—with no adjustments—with the “fit values’’ ( 3 . 0 , 1 . 1 , 1 . 7 ) quoted in §8 within 1 σ .
(5) Conclusion
Preprints 174972 i166

Appendix T.9 Determination and Theoretical Placement of the Reference Scale v ew

To map the exponential law m f , i = Y f , i i v ew / 2 into units of [GeV], the Higgs vacuum expectation value v ew | H | must be fixed. This section demonstrates, through a two-step procedure,
* (i) Experimental determination on the Standard-Model side (via the muon-decay constant G F ), * (ii) First-principles reproduction on the IFT–UEE side (using the tension σ ( μ ) and the Φ –loop effective action derived in Appendix E),
that
v ew = 246.22 GeV
emerges inevitably.
(1) Standard Model: Determination from the Muon-Decay Constant G F
The PDG 2025 empirical value
G F = ( 1.166 378 7 ± 0.000 000 6 ) × 10 5 GeV 2
already includes electroweak loop corrections. Inverting the tree-level formula
G F = 1 2 v ew 2
gives
v ew = ( 2 G F ) 1 / 2 = 246.21965 ± 0.00006 GeV ,
namely
v ew = 246.22 GeV .
(2) IFT–UEE: First-Principles Reproduction from σ and the Φ –Loop
(a) IR fixed point of the tension σ * .
From Appendix E.6, β σ = a σ 2 + b σ 3 , and the zero of β σ ( σ * ) = 0 is
σ * = a b = 118 ± 1 GeV 2 ( σ * = 10.9 ± 0.2 GeV ) ,
which sets the normalization point of the Φ –loop effective potential, Λ * 2 σ * .
(b) α Φ and ε ( μ ) .
Using Eq. (E.3), α Φ ( σ ) = κ Φ σ / σ 0 , κ Φ = 2 . 100 ± 0 . 004 , σ 0 = ( 440 MeV ) 2 , gives
α Φ ( σ * ) = κ Φ σ * / σ 0 = 51.8 ± 1.3 .
Although ε ( μ ) = exp [ 2 π / α Φ ( σ ( μ ) ) ] takes the value ε ( M Z ) = 5 . 06 × 10 2 at μ = M Z , only α Φ ( σ * ) enters the following estimate of v eff .
(c) Extremum of the effective potential v eff .
The 1-loop value of the four-point coupling obtained via the Green–Kubo integrals in Appendix E.3 is λ Φ ( Λ * ) = 0 . 0506 ± 0 . 0004 . With μ Φ 2 = α Φ ( σ * ) σ * ,
v eff = μ Φ 2 2 λ Φ = α Φ ( σ * ) σ * 2 λ Φ = 246.1 ± 3.5 GeV .
Thus v eff v ew is reproduced with no free parameters.
(3) Summary: Agreement of Experimental and Theoretical Values
Preprints 174972 i167

Appendix T.10 Summary

(1) Logical Chain Established in This Appendix
1)
Introduction of the normalised information measure L ˜ = ln det ( Y f Y f ) / K ( σ ) (Sec. T.2) and its dynamical relaxation L ˜ 0 by the resonance kernel R .
2)
First-principles calculation of fluid transport coefficients A common cutoff yields γ = 2 λ ˜ σ , η = 1 2 λ ˜ σ and the universal, cutoff-independent ratio α 0 = γ / η = 4 (Sec. T.3).
3)
Critical condition γ 2 η σ 0 = 0 Combined with σ 0 = C 0 n 2 , uniquely fixes
κ ˜ f ( σ ) = 1 v 3 α 0 σ 2 C 0 ε 1 2 O f
(Sec. T.4).
4)
Uniqueness of the integer matrix O f ILP yields ( O u , O d , O e ) = ( 7 , 11 , 8 ) as the unique minimum-trace solution (Sec. T.5).
5)
Determinant preservation and the normalisation factor With K ( σ ) = α 0 σ / ( 2 C 0 v 6 ) 3 ε O f one has det ( Y f Y f ) = K ( σ ) for all scales (Sec. T.5).
6)
Determination of the tension β -function β σ = a σ 2 + b σ 3 , a = 0 . 0760 GeV 2 , b = 6 . 43 × 10 4 GeV 4 with UV asymptotic freedom and the IR fixed point σ * = 118 GeV 2 (Sec. T.6).
7)
σ -dominated RG structure Chain rule implies g i ( μ ) = const . and G 1 = 4 σ ( μ ) (Sec. T.7).
8)
Verification of experimental consistency All nine masses and six mixing angles are grounded in first-principles inputs.
(2) Overall Synthesis
Preprints 174972 i168

Appendix U Appendix: First-Principles Derivation of the Exponential Law and ILP

Appendix U.1 Introduction: Role and Position of This Appendix

In Appendix E we derived
Y f ( μ ) = κ ˜ f ε O f ( μ )
from first principles, organising the scale dependence of the Yukawa matrices so that only the dimensionless normalisation constant κ ˜ f and the topological constant ε remain.
However, the **exponential matrix O f ** and the **exponential law itself** that generates it were still supplied externally.
The aims of Appendix F are reduced to the following two points:
1)
Using the quantum-vortex network and tension quantisation, derive O f Mat 3 × 3 ( Z ) ab initio from an integer linear programming (ILP) problem.
2)
With the unique solution O f thus obtained, rigorously prove the exponential law
Y f ( Λ IR ) = κ ˜ f ε O f
and, by coupling it with κ ˜ f , ε from Appendix E, complete the IFT as a truly parameter-free theory.
The only external datum required in this process is the high-energy reference scale Λ * . Once this is calibrated experimentally, κ ˜ f and ε are fixed immediately, and together with the O f and exponential law provided in this appendix, all masses and mixing angles are generated automatically.
(1) Structure of This Appendix
  • F.2  Sigma-Dominated RG and the Tension–Vorticity Dual Mapping
  • F.3  Vortex-Flux Quantisation and Integer Constraints
  • F.4  Free-Energy Minimisation ⟹ ILP
  • F.5  Existence and Uniqueness of the ILP Solution and the Necessity of g = 3
  • F.6  Enumeration of Exponential Matrices O f and CKM Consistency
  • F.7  The Exponential-Law Integration Theorem and Theoretical Error Estimates
Preprints 174972 i169

Appendix U.2 Scaling Law of the Fermion Fluid and Sigma-Dominated RG

In this section we recap the anisotropic scaling symmetry exhibited by the fermion-fluid action S [ ψ ] and the structure of the fixed point
T μ ν = Λ * 2 G μ ν
at which the tension tensor satisfies β σ = 0 . We then outline the mechanism by which the combination of RG flow and topological constraints produces integral quantisation conditions , thus preparing the groundwork for constructing the ILP in the subsequent sections.
(1) Fermion-Fluid Action and Scaling Transformation
Definition A146
(Fermion-Fluid Action [490] (Sec. 2.2, Definition 2.6)). For a fermion field ψ a ( t , x ) ( a = 1 , 2 , 3 generations)
S [ ψ ] = d t d 3 x i ψ ¯ γ 0 t ψ i v F ψ ¯ γ i i ψ σ ψ ¯ ψ ,
where v F is the fluid Fermi velocity and σ is the tension density . (The above is a reduced form of the full action Ψ ¯ ( i D Φ ) Ψ 1 3 σ + L GKLS + 2 π σ R sc listed in [490] (Eq. (5)), obtained in the flat-space, Φ = 0 gauge and non-dissipative limit as a low-energy three-dimensional representation.)
Scaling transformation.
Under
( t , x ) ( t , x ) = ( b z t , b x ) , b > 0 , z R ,
and taking the canonical dimension of ψ as [ ψ ] = d + z 1 2 , the kinetic term remains invariant with S b ( d + z 1 ) S . Requiring invariance of the tension term σ ψ ¯ ψ fixes [ σ ] = z , so that
σ ( μ ) = μ z σ ^ ( μ : RG scale ) .
(2) Sigma-Dominated RG and the Fixed Point β σ = 0
Lemma A211
(Existence of the Tension Fixed Point (Appendix E, Eq. E.37)). The β -function of σ ( μ ) , β σ = μ μ σ , is
β σ ( μ ) = z σ λ * 2 π 2 σ 3 + O ( σ 5 ) ,
where λ * is a positive finite constant. Thus a non-trivial solution of β σ = 0 exists at σ * = 2 π 2 z λ * , defining the scale μ = Λ * .
Proof. 
Equation (F.2.4) comes from extremising the one-loop effective potential V eff ( σ ) via V eff = 0 . Besides σ = 0 , one finds a positive root; verifying V eff ( σ * ) > 0 confirms its stability.     □
Theorem A132
(Recap of the Tension–Curvature Equivalence). At the fixed point σ *
T μ ν = Λ * 2 G μ ν ,
holds point-wise.
Proof. 
(i) Using the variation T μ ν = 2 δ S / δ g μ ν from Appendix D, Thm. D.38; (ii) inserting σ ( Λ * ) = σ * from Lemma A211; (iii) setting z = 1 yields σ * 2 = G Λ * 2 , which rearranges to (F.2.5).     □
(3) Mechanism by Which the RG Flow Generates Integral Quantisation
Definition A147
(Tension–Vorticity Dual Mapping [493]). A linear perturbation δ σ ( x ) near the fixed point corresponds isomorphically to the vorticity field ω ( x ) = × v via δ σ = Λ * ω .
Lemma A212
(Vortex-Flux Quantisation and the RG Integer Condition). The vortex flux around any closed loop C R 3 , Φ = C v · d x , satisfies Φ 2 π / m f Z ( m f : fermion mass). Elevating to Λ * under the RG flow yields
n = Φ 2 π / m f = δ σ Λ * / m f Z ,
i.e. δ σ / Λ * is necessarily integral.
Proof. 
The first statement follows from standard superfluid helicity quantisation with v = 1 m f θ . For the second, apply Definition A147, δ σ = Λ * ω , and use Stokes’s theorem Φ = ω · d S .     □
Theorem A133
(RG Integral Quantisation Theorem). In sigma-dominated RG, the tension perturbation obeys the discrete spectrum δ σ k = n k Λ * / m f with n k Z , providing the integer right-hand vector for the ILP constructed in later sections.
Proof. 
By Lemma A212, δ σ / Λ * Z . Decomposing δ σ = k n k ϕ k ( x ) , each coefficient n k is integral. Because ϕ k form a basis, integrality is preserved under basis changes, uniquely fixing the right-hand vector of the ILP.     □
Preprints 174972 i170

Appendix U.3 Vorticity–Tension Dual Mapping and the Flux-Quantisation Condition

In this section we rigorously define the correspondence map Φ between tension-concentrated regions and quantum vortex lines, and prove how the circulation quantisation
C v · d l = 2 π n m f
generates integral constraints . Furthermore, we derive Lemma F.3.4 , which shows that the first homology group of the vortex-line complement, H 1 ( Σ g , Z ) , is in one-to-one correspondence with the coefficient matrix of the ILP.
(1) Dual Map Φ between Tension Concentration and Quantum Vortex Lines
Definition A148
(Tension-Concentrated Region and Vortex-Line Complement). For the tension-density field σ ( x ) in a fermion fluid, define the region that exceeds the critical value σ c = σ * + δ σ by D = { x R 3 σ ( x ) σ c } . Quantum vortex lines γ R 3 form along the axis of the boundary D [493]. The three-dimensional space with vortex lines removed, Σ g = R 3 i = 1 g γ i , is called the vortex-line complement .
Definition A149
(Tension–Vorticity Dual Map). Define Φ : π 0 ( D ) { γ i } i = 1 g as
Φ : connected component D i vortex line γ i ,
where π 0 ( D ) is the set of connected components.
Theorem A134
(Bijectivity of the Dual Map Φ ). Imposing the critical-tension condition σ ( γ i ) = σ c makes the map Φ a bijection.
Proof. 
(Surjective) For each vortex line γ i there exists a tubular neighbourhood N ( γ i ) where σ ( x ) = σ c on the boundary; its interior collapses to a unique point in D i [493] (Th. 2). (Injective) If two distinct components D i D j produced the same vortex line, continuity would require D i D j , which is a contradiction. Hence Φ is injective.     □
(2) Flux Quantisation and the Origin of Integer Constraints
Lemma A213
(Vortex-Flux Quantisation [494] (§4)). For any closed curve C
C v · d l = 2 π m f n , n Z .
Proof. 
With the phase field θ = arg ψ one has v = 1 m f θ . Because θ is multi-valued up to θ θ + 2 π n , θ · d l = 2 π n , yielding (F.3.1).     □
Theorem A135
(Integrality of Tension Perturbations). Under the dual map Φ , the tension perturbation δ σ i associated with a vortex line γ i satisfies δ σ i = n i Λ * / m f , n i Z .
Proof. 
Extend Lemma A213 by Stokes’s theorem over the vortex surface S i : S i ω · d S = 2 π n i / m f . Using the dual map (Definition A149) and δ σ = Λ * ω , one obtains S i δ σ = n i Λ * / m f . Assuming axial symmetry makes δ σ constant on S i , giving the stated result.     □
(3) The Homology Group H 1 ( Σ g , Z ) and the ILP Coefficient Matrix
Lemma A214
(First Homology Group of the Vortex-Line Complement). The vortex-line complement Σ g is homeomorphic to a g-handlebody knot complement, hence
H 1 ( Σ g , Z ) Z g .
Proof. 
By deformation retraction, each vortex line γ i is surrounded by a torus tube T i S 1 × D 2 , and Σ g collapses to a g-handlebody. The standard homology calculation for a handlebody [495] (Prop. 3.1) gives (F.3.2).     □
Lemma A215
Lemma A66 (Homology Basis and the ILP Coefficient Matrix). Choose a basis [ C 1 ] , , [ C g ] for H 1 ( Σ g , Z ) and define a i j = Lk ( C i , γ j ) as the linking number with the vortex line γ j . The matrix A = ( a i j ) Mat g × g ( Z ) is an invertible integer matrix and is uniquely fixed as the coefficient matrix of the ILP A n = b .
Proof. 
(i) The linking number is a bilinear map Lk : H 1 ( Σ g ) × H 1 ( Σ g ) Z , and preserves det A = ± 1 under basis transformations [496] (Ch. 5). (ii) With the integer vector n = ( n 1 , , n g ) from Theorem A135 and the tension-perturbation integrals b = ( δ σ 1 , , δ σ g ) , one has A n = b , so A serves as the ILP coefficient matrix.     □
Preprints 174972 i171

Appendix U.4 Construction of the ILP from the Free-Energy Minimisation Principle

In this section we subdivide the tension-line network of the fermion fluid as
γ i j | 1 i j 3 , ( total number = 9 )
and identify each vortex-flux multiplicity n i j Z 0 with the components of the exponential matrix O f = ( O f ) i j via ( O f ) i j = n i j . The aim is to derive
min Tr O f = i = 1 3 ( O f ) i i ,
as a problem of free-energy minimisation and to reduce it to an integer linear programme (ILP).
(1) Free-Energy Functional for Bundled Flux Paths
Definition A150
(Free-energy functional F O f ).
F O f = 1 i j 3 α i j n i j + β Φ n i j 2 + ( i , j ) < ( k , ) γ Lk ( γ i j , γ k ) n i j n k ,
where i j is the shortest length of the vortex line γ i j , Φ = 2 π / m f is the unit flux, and the coefficient hierarchy α β γ is guaranteed by the sigma-dominated RG flow [497].
(2) Linearisation in the One-Term-Dominated Limit
Lemma A216
(Dominance of the linear term). In the limit α / β , α / γ , one obtains F [ O f ] = α i j i j n i j + O ( β , γ ) .
Proof. 
In Definition A150 the β - and γ -terms are suppressed relative to the α -term by factors O ( β / α ) and O ( γ / α ) . Taking the limit yields the claim.     □
(3) Formulation of the ILP (9 variables)
Vectorisation of variables.
x = n 11 , n 22 , n 33 , n 12 , n 21 , n 23 , n 32 , n 13 , n 31 Z 0 9 .
Objective function.
Retaining only the linear term via Lemma A216 and normalising the line lengths i j basis-wise gives
c x = n 11 + n 22 + n 33 = Tr O f .
Constraints.
* **Flux quantisation** (F.3.1)   A ( flux ) x = b ( flux ) (extended 9 × 9 linking-number matrix, with fixed det = ± 1 ).
* **CKM integer-difference conditions** [Eq. (8.3.4)]
| n 12 n 21 | = 1 , | n 23 n 32 | = 2 , | n 13 n 31 | = 3 .
Each absolute value is split into a positive–negative pair, rewritten as linear inequalities of the form B x = d , 0 x u .
Definition A151
(9-variable ILP).
min x Z 0 9 c x subject to A ( flux ) x = b ( flux ) , B x = d , 0 x u .
(4) Equivalence between Free-Energy Minimisation and the ILP
Theorem A136
(Free energy ⟺ 9-variable ILP). In the one-term-dominated limit, minimising the free energy
min O f Z 0 3 × 3 F [ O f ]
is fully equivalent to solving the 9-variable ILP given in Definition A151.
Proof. 
By Lemma A216, F [ O f ] is proportional to α c x ; since α > 0 , minimising one minimises the other. Flux quantisation and the CKM differences are expressed as the linear equalities (F.3.2) and (F.4.3). Therefore minimising F is equivalent to solving ILP (F.4.4).     □
(5) Reaffirming Minimum Trace as Tension-Length Saving
Lemma A217
(Trace and Tension Length (9-variable version)). The total tension-line length L tot = i j i j n i j is monotonically related to Tr O f .
Proof. 
Since i j > 0 are fixed constants,
L tot min i j i j i j n i j min i i i Tr O f .
    □
Theorem A137
(Physical meaning of the minimum-trace principle). Minimising the optimal value Tr O f of ILP (F.4.4) is equivalent to shortening the leading free-energy term α L tot , i.e. to saving the total length of bundled tension lines .
Proof. 
Direct from Lemma A217 with α > 0 .     □
Preprints 174972 i172

Appendix U.5 Existence and Uniqueness of the ILP Solution: Integer-Solution Theorem

For the 9-variable ILP formulated in F.4
min x Z 0 9 c T x s . t . A x = b , B x = d ,
with
x = ( x 11 , x 22 , x 33 , x 12 , x 21 , x 23 , x 32 , x 13 , x 31 ) T ,
we prove that it possesses a unique non-negative integer solution . The optimal solution satisfies the CKM differences | x 12 x 21 | : | x 23 x 32 | : | x 13 x 31 | = 1 : 2 : 3 , and reproduces Table 8.2 of Chap. 8 exactly.
(1) Smith Normal Form of the Linking-Number Matrix
Definition A152
(Linking-number matrix A Mat 9 × 9 ( Z ) ). Each entry is defined by A p q = Lk ( C p , γ q ) , using the vortex-line basis { γ i j } i j and the homology basis { C p } p = 1 9 extended in F.3.
Proposition A1
(Smith normal form). The matrix A is invertible with det A = ± 1 , so there exist U , V GL ( 9 , Z ) such that U A V = I 9 .
Proof. 
By the Milnor–Turaev torsion theorem using complete bilinearity and a mutually dual basis [495], det A = ± 1 . Since A is an invertible integer matrix, its Smith normal form has invariant factors d i = 1 , hence I 9 .     □
(2) Right-Hand Vector and CKM Difference Constraints
Lemma A218
(Right-hand vector). At the fixed point β σ ( Λ * ) = 0 one has b = ( 1 , 0 , 0 , 0 , 0 , 0 , 0 , 0 , 0 ) T .
Definition A153
(CKM difference matrix).
B = 0 0 0 1 1 0 0 0 0 0 0 0 0 0 1 1 0 0 0 0 0 0 0 0 0 1 1 , d = ( 1 , 2 , 3 ) T .
The absolute values have already been fixed to the upward-flux orientation by Lemma F.4.3.
(3) Uniqueness of the ILP Solution
Lemma A219
(Extraction of the single candidate). Applying U A V = I 9 and transforming variables with y = V 1 x , one obtains
I 9 y = e 1 , B ˜ y = d , B ˜ = B V .
Solving these equations in integers yields the unique solution y = e 1 .
Proof. 
The equation I 9 y = e 1 enforces y 1 = 1 , y 2 9 = 0 . To satisfy B ˜ e 1 = d , the first column of B ˜ must be ( 1 , 2 , 3 ) T with all other columns vanishing, which can always be arranged by an appropriate choice of the linking basis (Chap. 8, Lem. 8.1).     □
Theorem A138
(Integer-solution theorem (revised)). The ILP (F.5.0) has exactly one non-negative integer solution,
x = ( 5 , 2 , 0 , 5 , 6 , 1 , 3 , 2 , 5 ) T
Proof. 
Lemma A219 gives y = e 1 . Reverting to the original variables, x = V e 1 , which is integer and non-negative. Definition A153 shows that B x = d . Invertibility and the non-negativity constraint ensure uniqueness.     □
Corollary A6
(Satisfaction of the difference conditions). With solution (F.5.1)
| x 12 x 21 | = | 5 6 | = 1 , | x 23 x 32 | = | 1 3 | = 2 , | x 13 x 31 | = | 2 5 | = 3 ,
which matches exactly Eq. (8.3.4) of Chap. 8.
(4) Necessity of Three Generations g = 3
Lemma A220
(Free rank). The free homology rank of the vortex-line complement is g = rank H 1 ( Σ g ) = 3 .
Corollary A7
(Fixing the number of generations). The smallest g for which both the integer quantisation (Lemma A220) and the anomaly-cancellation conditions f Q f = f Q f 3 = 0 are simultaneously satisfied is g = 3 .
Preprints 174972 i173

Appendix U.6 Determination of the Exponential Matrices O f and the Minimum-Trace Principle

Using the unique solution of the 9-variable ILP obtained in F.5
x = ( 5 , 2 , 0 , 5 , 6 , 1 , 3 , 2 , 5 ) T x 11 , x 22 , x 33 , x 12 , x 21 , x 23 , x 32 , x 13 , x 31 ,
we determine the exponential matrices O f for each fermion species f { u , d , e } and show that
| ( O u ) 12 ( O d ) 12 | : | ( O u ) 23 ( O d ) 23 | : | ( O u ) 13 ( O d ) 13 | = 1 : 2 : 3 ,
coinciding with Eq. (8.3.4) of Chap. 8.
(1) Construction of the Matrix O u
Definition A154
(Upper-generation matrix O u ).
O u = 5 5 2 6 2 1 5 3 0 , Tr O u = 7 .
Rows/columns are assigned by placing ( x 11 , x 22 , x 33 ) on the diagonal and the off-diagonals in the sequence ( x 12 , x 21 , x 23 , x 32 , x 13 , x 31 ) .
(2) Construction of O d and CKM Differences
Definition A155
(Lower-generation matrix O d ). Set O d = O u + Δ , with
Δ = 2 1 3 0 1 2 0 2 1 .
Hence
O d = 7 6 5 6 3 3 5 1 1 , Tr O d = 11 .
Lemma A221
(CKM consistency).
| ( O u ) 12 ( O d ) 12 | , | ( O u ) 23 ( O d ) 23 | , | ( O u ) 13 ( O d ) 13 | = ( 1 , 2 , 3 ) .
Proof. 
Taking the differences gives ( 5 6 , 1 3 , 2 5 ) = ( 1 , 2 , 3 ) ; absolute values yield the claim.     □
(3) The Lepton Matrix O e
Following the symmetric-degeneracy condition ( θ 12 PMNS θ 23 PMNS ) of Chap. 8 §8.4 and minimising the trace to 8, we obtain
O e = 5 4 2 4 3 1 2 1 0 , Tr O e = 8 .
(4) Commutative Diagram: ILP → RG → Dimensionless Yukawa
Lemma A222
(ILP → RG correspondence). Each component ( O f ) i j corresponds one-to-one to the tension perturbation δ σ i j = ( O f ) i j Λ * / m f .
Lemma A223
(RG → dimensionless Yukawa matrix). Integrating the RG equation μ μ Y f = β Y f ( Y f , σ ) gives
Y f ( Λ IR ) = κ ˜ f ε O f ,
where κ ˜ f is the dimensionless normalisation constant of Appendix E (Eq. E.24).
Lemma A224
(Diagram Lemma F.6.2).
Preprints 174972 i186
is commutative (L = Lemma A222, R = Lemma A223).
Proof. 
One has R L ( O f ) = κ ˜ f ε O f , coinciding with the image of L followed by R.     □
(5) Diophantine Stability
Theorem A139
(Diophantine stability). For any perturbation with Δ A < 1 , the integer solution of the ILP and the matrices O f remain unchanged.
Proof. 
A + Δ A retains det ( A + Δ A ) = ± 1 and is invertible. The invariant factors of its Smith normal form remain d i = 1 under continuous perturbations [498] (Th. 12.4). Since the right-hand vector b and the CKM differences are unchanged, the unique integer solution is preserved.     □
Preprints 174972 i174

Appendix U.7 Unified Theorem of the Exponential Law and Error Analysis

In this section we combine the integral quantisation of the tension strength and the uniqueness of the exponential matrices O f established in F.4–F.6 to derive, from first principles, that the dimensionless Yukawa matrices obey
Y f ( Λ IR ) = κ ˜ f ε O f
Moreover, we show that theoretical errors arising from higher-loop corrections are suppressed down to machine-round-off precision. (Hereafter, κ ˜ f denotes the dimensionless Yukawa normalisation constants at μ = Λ * determined in Appendix E.)
(1) Derivation of the Topological Constant ε
Definition A156
(Topological holonomy constant). The strong-coupling constant of the scalar phase field, α Φ ( σ ) , satisfies 1 / α Φ ( σ * ) Z > 0 when the tension is at the fixed-point value σ * (the monopole-quantisation condition of the tension–curvature duality). The associated phase holonomy is defined by
ε : = exp 2 π α Φ ( σ * )
with 0 < ε < 1 . The constant ε is topological and involves no external input.
Lemma A225
(Fixing the critical ratio). The topological constant ε sets the UV–IR scale separation as Λ IR = ε Λ * .
Proof. 
Define μ = Λ IR by matching the one-loop effective action of Φ , S 1 - loop ( 2 π / α Φ ) ln ( Λ * / μ ) , to the phase 2 π ; the resulting scale coincides with the stated relation.     □
(2) Logarithmic Lattice and Linearisation of the RG Flow
Definition A157
(Logarithmic lattice). L = { μ k = ε k Λ * k Z } is called the logarithmic lattice . It satisfies ln μ / ln ε Z .
Lemma A226
(Logarithmic linearisation). Integrating the RG equation μ μ Y f = γ f ( σ ) Y f along L gives
ln Y f ( μ k 1 ) Y f ( μ k ) = γ f ( σ k ) ln ε , γ f ( σ k ) Q .
Proof. 
The interval length is ln ε . Because the tension spectrum is σ k = n k Λ * / m f (result of F.3), γ f ( σ k ) is rational.     □
(3) Exponentiation Lemma and the Integer Matrix O f
Lemma A227
(Exponentiation lemma). Summing (F.7.2) for k = 1 , , N with μ 0 = Λ * and μ N = Λ IR yields
ln Y f ( Λ IR ) Y f ( Λ * ) = k = 1 N γ f ( σ k ) ln ε = O f ln ε ,
where O f = k γ f ( σ k ) Z 3 × 3 is uniquely fixed by the ILP of F.5.
(4) Unified Theorem of the Exponential Law
Theorem A140
(Unified theorem of the exponential law). With the dimensionless constants κ ˜ f = Y f ( Λ * ) and the unique ILP solution O f ,
Y f ( Λ IR ) = κ ˜ f ε O f .
Proof. 
Lemma A227 gives ln Y f ( Λ IR ) = ln κ ˜ f + O f ln ε . Exponentiating yields the claim.     □
(5) Upper Bound on the Error
Lemma A228
(Suppression of higher-loop corrections). -loop corrections are suppressed as O ( ε + 1 ) , and 1 O ( ε + 1 ) < 10 12 for ε 0 . 05 .
Theorem A141
(Upper limit on the theoretical error).
Y f all - loop κ ˜ f ε O f Y f all - loop 10 12 ,
i.e. the theoretical uncertainty is at most the machine-round-off level.
Proof. 
Apply Lemma A228 to the matrix norm.     □
Preprints 174972 i175

Appendix V Appendix: Bridge from Single-Fermion Fluid to “Field Equations”

Appendix V.0 Executive Summary

The purpose of this Appendix G is to present in a single logical chain, (i) starting from the law of motion of an individual particle (Newton) , through (ii) coarse-graining via fluid dynamics , to (iii) the emergence of the “field equations” of electromagnetism, Yang–Mills, and gravity , all without circular reference. The UEE formalism (UEE_01–06) is introduced only in the minimally required places (derivation of minimal dissipation for open systems and the zero-area kernel), and it is explicitly shown from external principles why it becomes inevitable at those points (GKLS complete positivity, OS reflection positivity, measure-theoretic construction of the zero-area kernel). The construction follows the separately attached roadmap (M1–M6).
(1) Problem Setting and Requirements of Non-Circularity
Definition A158
(Microscopic Minimal Principles (G1–G3)).
1
Degrees of Freedom (G1) : Identical point particles i = 1 , , N have position x i ( t ) and velocity v i ( t ) , obeying Newton’s law of motion x ˙ i = v i , m i v ˙ i = F i .
2
Conservation Laws (G2) : Conservation of particle number, momentum, and energy holds.
3
Minimal Structure (G3) : The interaction is local, and one can define a tension scalar σ and a local phase as functions of the particle configuration, which contribute to the stress tensor upon coarse-graining.
The above are independent propositions without assuming a higher-level theory (UEE is introduced later in this section from external principles).
Definition A159
(Fluid Variables and Information Current). From the single-fermion field Ψ , define the information current four-vector J μ : = Ψ ¯ γ μ Ψ , and set
n : = J μ J μ , u μ : = J μ n ( u μ u μ = 1 )
as the fluid density and normalized four-velocity .
Lemma A229
(Time-positivity and Continuity Equation). Under J 0 > 0 , one has n > 0 and u μ u μ = 1 , and furthermore
μ ( n u μ ) = 0 ,
i.e. conservation of particle number (continuity equation).
Proof. 
Since J μ J μ = ( Ψ Ψ ) 2 + i ( J i ) 2 < 0 , we obtain n = J μ J μ > 0 , and u μ u μ = J μ J μ / n 2 = 1 . Substituting J μ = n u μ into the Noether current μ J μ = 0 , we obtain μ ( n u μ ) = 0 . Each step is standard for C -class Ψ .     □
(2) Emergence of U ( 1 ) Electromagnetic Field: Local Phase Invariance ⇒ Compensating Field
Theorem A142
(Minimal Coupling and Coulomb Law from Local Phase Invariance). The necessary and sufficient condition for dynamics to be invariant under local phase transformation Ψ e i θ ( x ) Ψ is the introduction of μ D μ : = μ + i A μ . Then the gauge field A μ is massless and in the static limit yields the potential V ( r ) = α / r .
Proof. 
(i) From unitary equivalence under e i θ , first-order variation requires [ θ , D ] = 0 . If μ θ 0 , one can cancel it by adding a compensating term A μ , defining D μ = μ + i A μ . (ii) The mass term 1 2 m γ 2 A μ A μ is not invariant under A μ A μ μ θ , hence excluded ( m γ = 0 ). (iii) The static limit of the massless propagator D μ ν ( k ) = i η μ ν / k 2 gives D 00 ( r ) = 1 / ( 4 π r ) by Fourier inversion. Multiplying by the charge coupling e 2 = 4 π α yields V ( r ) = α / r . This proves the claim.     □
(3) Emergence of Yang–Mills: Projection System of Internal Indices and Functional Completeness
Definition A160
(Five-Operator System S 5 and Mapping). Let S 5 : = { D , Π n , V n , Φ , R } be the functionally complete system of a single fermion ( V n = γ Π n , R the zero-area resonance kernel). A bijection G : Φ ( D , Π n , V n , R ) exists between Φ and S 5 .
Theorem A143
(Functional Completeness and Recovery of Standard Model Gauge Group). S 5 is functionally complete, and through the orthogonal projection family Π n , the gauge structure S U ( 3 ) c × S U ( 2 ) L × U ( 1 ) Y is faithfully realized. Removing any of the elements of S 5 breaks at least one functional requirement.
Proof. 
(Sketch) D , Φ generate C l ( 1 , 3 ) and its commutative subalgebra. Adding the projection system { Π n } corresponding to finite group actions yields a semidirect product algebra. With V n generating the GKLS semigroup, the full set of locally bound operators becomes accessible. R fixes curvature term coefficients and closes the equivalence among the three forms (action, operator, field equation). Removal experiments show that at least one requirement (unitarity/CPTP/measurement basis/GR reduction/BH information retention) fails in each case.     □
(4) Emergence of Gravity: Stress–Curvature Equivalence and Newtonian Limit
Definition A161
(Stress Tensor and Tension Scalar). Let T μ ν be the fluid stress obtained from variational principle, and define the coupling constant using the tension scalar σ as Λ * 2 : = 2 π / σ .
Theorem A144
(Stress–Curvature Equivalence). From metric variation one obtains
T μ ν = Λ * 2 G μ ν , Λ * 2 = 2 π σ .
Thus μ T μ ν = 0 is equivalent to the Bianchi identity.
Proof. 
Consider the action
S IFT = Ψ ¯ ( i D Φ ) Ψ 1 3 σ + L GKLS + 2 π σ R sc g d 4 x .
Variation of the matter term gives 1 2 T μ ν δ g μ ν g d 4 x , and variation of the curvature term gives 2 π σ G μ ν δ g μ ν g d 4 x . With boundary conditions (Dirichlet or no-boundary), the boundary term vanishes. Stationarity condition equates the coefficients of the integrands, establishing the claim.     □
Lemma A230
(Newtonian Limit and Inverse-Square Law). In the weak-gravity, low-velocity limit g μ ν = η μ ν + h μ ν with | h μ ν | 1 , taking h 00 = 2 Φ N recovers 2 Φ N = 4 π G ρ eff , i.e. the inverse-square law.
(5) Where the UEE Formalism Becomes Inevitable: Minimal Dissipation of Open Systems and Kernel R
Theorem A145
(Uniqueness of GKLS Minimal Dissipation and Measure Theory of Zero-Area Kernel). The open-system dynamics obtained by coarse-graining is uniquely specified in the minimal form that satisfies complete positivity, trace preservation, gauge/gravity covariance, and OS reflection positivity , namely GKLS (Lindblad) (with V n = γ Π n , rank C L = 18 minimal). Furthermore, from the limit of information-current cut-off , the zero-area resonance kernel R can be defined:
R A e λ A , Tr [ R ρ ] = 0 , H 2 ( supp Π R ) = 0 .
Thus the threefold equivalence (operator, variational, field equation) is closed, and the coefficients of Theorem A144 are fixed.
Proof. 
(i) Canonical form of GKLS: the form simultaneously minimizing Choi–Kraus rank and satisfying completeness n V n V n = γ 1 is uniquely equivalent to V n = γ Π n (up to phase freedom), with rank C L = 18 . (ii) R kernel: when the support set of information-current cut-off boundaries degenerates to H 2 = 0 , R can be defined axiomatically, equivalent to the zero-area condition ( H 2 = 0 arbitrarily small-area C 1 approximations). (iii) It follows that the R of UEE/IFT is identical (up to phase freedom).     □
(6) Overall Logic of This Appendix and Consistency with Previous Results
The tools used in this section (functional completeness of S 5 , threefold equivalence, T μ ν = Λ * 2 G μ ν ) connect systematically to the rigorous proofs in the main text (Chaps. 2–3, 11, etc.) and UEE_06 (§1.1–1.3, §2.1–2.4), ensuring consistency of Standard Model reproduction and GR limit (see main text for figures and details of removal experiments).
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Appendix V.1 Microscopic “Minimal Principles”: Newtonian Motion of Elementary Particles and Conservation Laws

(1) Purpose and Stance
In this section, without assuming any introduction of fields , we adopt solely Newtonian mechanics of identical elementary particles (point-mass approximation, finite mass) as the starting point, and rigorously derive the global conservation laws (total particle number, total linear momentum, total angular momentum, total energy) together with the local continuity equation for particle-number conservation . As a conclusion , the minimal set of principles (M1)–(M3) is established that enables a consistent bridge to coarse-graining (continuum approximation) in the subsequent Sec. G.2. The fluid skeleton constructed here ( n , u μ and the continuity equation) corresponds isomorphically to the definition of information current in IFT, J μ : = Ψ ¯ γ μ Ψ with n : = J μ J μ , u μ : = J μ / n (to be cross-checked in Sec. G.2)6.
(2) Definition of the System and Minimal Axioms (M1–M3)
Definition A162
(Microscopic System and Kinematics). Consider a system consisting of N N point particles of identical mass m > 0 . The position and velocity of each particle are given by
x i : R R 3 , v i ( t ) : = x ˙ i ( t ) ( i = 1 , , N ) .
Definition A163
(Dynamics and Interaction (Minimal Principles)). The minimal principles used in this section are summarized in (M1)–(M3) below.
(M1)
(Newton’s Equations of Motion) Each particle obeys
m v ˙ i ( t ) = F i ( t ) .
(M2)
(Action–Reaction, Central Forces) The interaction can be written as the sum of pairwise forces F i = j i F i j + F i ext , with F i j = F j i and F i j = f i j ( r i j ) r ^ i j ( r i j : = | x i x j | , r ^ i j : = ( x i x j ) / r i j ).
(M3)
(Symmetries and Conservation-Law Premise) A potential V ( x 1 , , x N ) exists and satisfies homogeneity in time and space as well as rotational symmetry (hence, by Noether’s theorem, conservation of total energy, total linear momentum, and total angular momentum is available).
(3) Rigorous Derivation of Global Conservation Laws
Lemma A231
(Conservation of Total Linear Momentum). The total linear momentum P ( t ) : = i = 1 N m v i ( t ) is constant; that is, P ˙ ( t ) = 0 .
Proof. 
P ˙ = i m v ˙ i = i F i = i j i F i j + i F i ext .
For the internal forces, F i j = F j i implies i j i F i j = 0 . If the external force vanishes for the whole system (isolated system), then i F i ext = 0 , hence P ˙ = 0 .     □
Lemma A232
(Conservation of Total Angular Momentum). The total angular momentum L ( t ) : = i x i ( t ) × m v i ( t ) is constant.
Proof. 
L ˙ = i x ˙ i × m v i + i x i × m v ˙ i = i x i × F i ,
where the first term vanishes because v i × m v i = 0 . For the internal-force contribution,
i x i × j i F i j = 1 2 i j ( x i x j ) × F i j .
By the central-force assumption F i j ( x i x j ) , each term vanishes; hence L ˙ = 0 (assuming an isolated system).     □
Lemma A233
(Conservation of Total Energy). When V has no explicit time dependence, the total energy E : = i 1 2 m | v i | 2 + V ( x 1 , , x N ) is constant.
Proof. 
E ˙ = i m v i · v ˙ i + i x i V · x ˙ i = i F i · v i i F i ( pot ) · v i = 0 ,
where F i ( pot ) : = x i V , we set F i = F i ( pot ) , and used time invariance.     □
(4) Local Representation: Particle-Number Density and Continuity Equation
As the starting point for local conservation laws, define the microscopic particle-number density and microscopic particle flux by
ρ mic ( x , t ) : = i = 1 N δ x x i ( t ) , j mic ( x , t ) : = i = 1 N v i ( t ) δ x x i ( t ) .
Theorem A146
(Continuity Equation for Particle-Number Conservation). In the distributional sense,
t ρ mic ( x , t ) + · j mic ( x , t ) = 0
holds identically.
Proof. 
Let φ C c ( R 3 ) be arbitrary. From Definition (A41),
t ρ mic , φ = t i φ x i ( t ) = i φ x i ( t ) · x ˙ i ( t ) = R 3 φ ( x ) · j mic ( x , t ) d 3 x .
By integration by parts, t ρ mic , φ = · j mic , φ . Hence (A42) holds as a distribution.     □
Lemma A234
(Coarse-Graining and Mapping to the Fluid Skeleton (Preparation)). With a spatial smoothing kernel W ( x ) 0 ( W = 1 , a mesoscale), define the convolutions
n ( x , t ) : = ( ρ mic * W ) ( x , t ) , u ( x , t ) : = ( j mic * W ) ( x , t ) n ( x , t ) .
Then Theorem A146 isomorphically becomes t n + · ( n u ) = 0 (no limit is required with fixed ).
Proof. 
Convolve (A42) with W and use the commutation of t and with convolution and linearity; the claim follows immediately.     □
Remark (Cross-Check with IFT)
The above n , u correspond to the classical limit of the hyperbolic normalization of J μ in IFT, n : = J μ J μ and u μ : = J μ / n , and the continuity equation coincides with the theorem (particle-number conservation) in UEE_067. This correspondence will be lifted to tensorial form and used in the subsequent Sec. G.2.
(5) Summary of the “Minimal Principles” Established in This Section
From the above, the following non-circular, minimal assumptions and conclusions have been established:
(M1)
Newtonian motion (Definition A163).
(M2)
Action–reaction and central forces (Definition A163).
(M3)
Homogeneity of time and space and rotational symmetry (Definition A163).
From these, (i) conservation of total linear momentum, total angular momentum, and total energy (Lemmas A231, A232, A233), and (ii) local particle-number conservation (Theorem A146) have been derived line-by-line . Up to this point, the discussion has not assumed the UEE formalism at all (UEE will be introduced inevitably in G.6 from the minimal requirements of coarse-graining = open systems8).
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Appendix V.2 Coarse-Graining from Many-Body to Fluid: Continuity, Euler, and Vorticity

(1) Aim and Position
In this section, starting from the microscopic degrees of freedom of the single-fermion fluid (IFT), we from first principles derive, via coarse-graining, the standard fluid equations (continuity equation, Euler equation, vorticity equation), and embed, in a form consistent with conservation laws, the effects of dissipation introduced in the UEE-IFT formalism (GKLS type) and of the zero-area resonance kernel R. The framework is presented along two routes: (A) a coarse-grained derivation from the Newtonian motion of a microscopic many-body system, and (B) a coordinated derivation from the IFT conservation equations μ ( n u μ ) = 0 , μ T μ ν = 0 , and their equivalence is proved in a theorem given below.
(2) Definition of the Coarse-Graining Operator and Field Variables
Coarse-graining is defined using a local averaging kernel W ( x ) (positive, C , W = 1 , even function, moments of order O ( 2 ) ).
Definition A164
(Empirical Measure and Coarse-Grained Fields). Consider a system of point particles with microscopic identifiers α = 1 , , N (mass m α , position q α ( t ) , velocity v α ( t ) ). For the empirical measure
μ N ( t , x ) : = α = 1 N δ ( x q α ( t ) ) ,
define the coarse-grained density, momentum density, and velocity by
ρ ( t , x ) : = α m α W ( x q α ( t ) ) ,
j ( t , x ) : = α m α v α ( t ) W ( x q α ( t ) ) ,
u : = j / ρ .
In the nonrelativistic approximation, the relation to the natural IFT variables ( n , u μ ) is ρ m n , and u coincides with the spatial velocity in IFT.
Lemma A235
(Continuity Equation (Exact Form for Finite under Coarse-Graining)). Assuming only the particle equations of motion q ˙ α = v α , one has
t ρ + · ( ρ u ) = 0 exactly .
Proof. 
If W has no time dependence, then
t ρ = α m α t W ( x q α ) = α m α q ˙ α · W ( x q α ) .
Also,
· ( ρ u ) = · α m α v α W ( x q α ) = α m α v α · W ( x q α ) .
Adding the two expressions yields zero, giving (A46). In IFT, the equivalent conservation equation μ ( n u μ ) = 0 holds.     □
(3) Derivation of the Euler Equation: Newtonian Limit and IFT Limit
Let F α be the force acting on particle α . The time evolution of the momentum density is
t j = α m α v ˙ α W α m α ( v α v α ) · W .
The first term on the right-hand side equals the coarse-grained force density f : = α F α W . The second term can be rewritten in the dissipative form of Reynolds stress.
Definition A165
(Decomposition of the Stress Tensor).
τ : = α m α ( v α u ) ( v α u ) W , Π : = ρ u u + τ .
Under the isotropic approximation τ p I , p becomes the coarse-grained pressure.
Theorem A147
(Euler Equation (Inviscid, with External Force)). When the external force density f is conservative, f = ρ Φ , one has
t ( ρ u ) + · ( ρ u u ) + p = ρ Φ .
Further, in the generalization including viscosity and damping (UEE-NS extension),
t u + ( u · ) u = 1 ρ p Φ + ν Δ u γ u ,
holds (with ν 0 the effective viscosity and γ 0 the damping).
Proof. 
From Definition A165,
t j + · Π = f .
Substituting the isotropized Reynolds stress τ p I and Π = ρ u u + p I , and supplementing (GKLS-origin) effective viscosity ν and damping γ as correction terms, yield (A47)–(A48). The Navier–Stokes extension with γ u is introduced rigorously in the UEE appendix (English edition).     □
Re-derivation from IFT and Origin of the Potential.
From IFT’s stress–curvature equivalence T μ ν = Λ * 2 G μ ν and the full form of the spinor-fluid stress T μ ν , in the nonrelativistic limit one obtains
( ε + p ) u μ μ u ν + ( δ ν + μ u ν u μ ) μ p = ( dissipation ) ,
(the time component is the continuity equation). Here p is determined via IFT’s tension scalar σ , and Φ is interpreted as an effective potential induced from σ (see the IFT main text for precise definitions and variational computations).
(4) Vorticity Equation and Baroclinic Term
Define the vorticity ω : = × u . Taking the curl of (A48) and using × Φ = 0 , we have
Lemma A236
(Vorticity Transport Equation (UEE-NS Form)).
t ω = × ( u × ω ) + ρ × p ρ 2 + ν Δ ω γ ω .
The second term on the right-hand side is the baroclinic term .
Proof. 
Use the vector identities × [ ( u · ) u ] = ( ω · ) u ( u · ) ω + ω ( · u ) , × ( ρ 1 p ) = ρ 1 × p = ( ρ × p ) / ρ 2 , and rearrange by the continuity equation (A46) (accounting for compressibility). Note that × ( γ u ) = γ ω and × ( ν Δ u ) = ν Δ ω .     □
IFT Tension σ and Vorticity Source.
When the pressure p is a local function of σ , p = p ( σ , ρ ) , one has p = p σ σ + p ρ ρ , hence
ρ × p ρ 2 = 1 ρ 2 p σ ( ρ × σ ) ,
i.e., spatial misalignment of σ (not parallel to the density gradient) produces a source of vorticity. This mechanism agrees with the derivation of the vorticity equation in IFT.
(5) Equivalence of the Two Routes (Many-Body Coarse-Graining ⇔ IFT)
Theorem A148
(Equivalence Theorem). (i) The equations (A46), (A48), (A49) obtained from a many-body Newtonian system with the coarse-graining and isotropization of Definition A164 (assumptions on W , bounded ), and (ii) the corresponding equations obtained from IFT conservation laws μ ( n u μ ) = 0 , μ T μ ν = 0 and the nonrelativistic limit of the IFT stress, give the same dynamics when ν , γ are chosen as effective coefficients consistent with UEE dissipation (GKLS) and the zero-area nature of R .
Proof. 
IFT’s spacetime conservation μ T μ ν = 0 yields, in the nonrelativistic limit, the structure of (A47) (pressure, potential, dissipation). The GKLS-type dissipation of UEE satisfies CPTP and OS reflection positivity, so it is possible to introduce viscosity and damping ( ν , γ ) compatible with the definitions of conserved quantities (charge, energy–momentum). The kernel R has zero-area (measure-zero) support and zero trace, and does not destroy the structure of conservation equations (for detailed operator relative-boundedness, see theorems of UEE). Therefore, by expressing the effective coefficients appearing in (i) by the dissipative parameters in (ii), the equation forms coincide.     □
(6) Conclusion of This Section (Key Points)
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Appendix V.3 Emergence of “Fields” I: U ( 1 ) Electromagnetic Field (Local Phase Invariance)

(1) Aim and Position
In this section, starting from the fundamental variables of the single-fermion fluid obtained in G.1 (Newtonian motion and conservation laws of elementary particles) and G.2 (coarse-graining from many-body to fluid),
J μ : = Ψ ¯ γ μ Ψ , n : = J μ J μ , u μ : = J μ n
(with u μ u μ = 1 , μ ( n u μ ) = 0 ), we rigorously derive, line by line and from both the action principle and the fluid representation, that the U ( 1 ) gauge field A μ and Maxwell’s equations arise inevitably from local phase invariance. The equivalence of the three forms (action, operator, and field equations) of the Unified Evolution Equation (UEE) adopted here, and the U ( 1 ) derivation within the single-fermion framework (IFT), are systematically provided in previous works. These constitute the basis for each proposition in this section (equivalence of the three forms of UEE and variational derivation of the gauge field, as well as the inevitability of U ( 1 ) from local phase invariance in IFT).
(2) Inevitability of the Connection from Local Phase Invariance
Definition A166
(Local U ( 1 ) Transformation and Covariance of the Density Operator). For a smooth real function θ ( x ) ,
Ψ ( x ) Ψ ( x ) : = e i θ ( x ) Ψ ( x ) , Ψ ¯ ( x ) Ψ ¯ ( x ) : = Ψ ¯ ( x ) e i θ ( x ) .
The necessary and sufficient condition for the UEE time evolution ρ ˙ = i [ D , ρ ] + L Δ [ ρ ] to be covariant under this transformation as ρ e i θ ρ e i θ is that the differential-operator part be replaced by μ D μ : = μ + i A μ , with the introduction of a connection A μ transforming as A μ A μ μ θ . Moreover, each jump operator V j of the Lindblad part L Δ must be a gauge scalar.
Lemma A237
(Uniqueness of Minimal Coupling). Under Def. A166, a reversible generator satisfying covariance under U ( 1 ) transformations is restricted to the form
D = i γ μ ( μ + i A μ ) +
(where “…” denotes gauge-scalar couplings). Adding a mass term 1 2 m γ 2 A μ A μ breaks gauge invariance, hence m γ = 0 .
Proof. 
For i [ D , ρ ] to define an isomorphism under ρ e i θ ρ e i θ , the correction D e i θ D e i θ + i e i θ t ( e i θ ) must be canceled by the contribution from spatial derivatives of θ . Since μ does not commute with θ , the introduction of D μ is necessary and sufficient. The mass term is not invariant under A μ A μ μ θ , and is therefore forbidden.     □
(3) Derivation of Maxwell’s Equations from the Action Principle
Definition A167
( U ( 1 ) –Dirac–Maxwell Action). In natural units,
S [ Ψ , Ψ ¯ , A ] : = d 4 x g Ψ ¯ i γ μ D μ m Ψ 1 4 F μ ν F μ ν , F μ ν : = μ A ν ν A μ .
In the variational form of UEE (UEEvar), this gauge sector is embedded in the standard way, and the dissipative term and the zero-area resonance kernel R are added as gauge scalars.
Theorem A149
(Field Equations). Varying the action of Def. A176 independently with respect to A ν and Ψ ¯ , Ψ , and imposing the boundary condition δ A μ | M = 0 , one obtains
μ F μ ν = j ν , j ν : = Ψ ¯ γ ν Ψ , ( i γ μ D μ m ) Ψ = 0
(with covariant derivatives in a curved background).
Proof. (line-by-line)
(i) Variation in A ν : δ S | A = g { Ψ ¯ ( i γ ν Ψ ) δ A ν 1 2 F μ ν ( μ δ A ν ν δ A μ ) } . By integration by parts and antisymmetry, δ S | A = g ( μ F μ ν j ν ) δ A ν . The boundary term vanishes under the boundary condition. Hence μ F μ ν = j ν .
(ii) Variations in Ψ ¯ , Ψ give the Dirac equation by standard computation. (In UEEvar, the Euler–Lagrange equations for the gauge sector are identical.)     □
Lemma A238
(Geometric Identity). Since F = d A , one has [ λ F μ ν ] = 0 (Bianchi identity). This is equivalent to μ F ˜ μ ν = 0 with F ˜ μ ν : = 1 2 ε μ ν ρ σ F ρ σ .
(4) Fluid Representation: Continuity Equation and Lorentz Force
Definition A168
(Fluid Variables). With J μ = Ψ ¯ γ μ Ψ , n = J μ J μ , u μ = J μ / n , one has μ ( n u μ ) = 0 and u μ u μ = 1 .
Theorem A150
(Fluid Form of the Equation of Motion (Lorentz Force)). With an appropriate stress–energy tensor T μ ν ,
μ T μ ν = F ν j ρ ρ , j ρ = n u ρ ,
i.e., the electromagnetic Lorentz force density appears in the equation of motion. In particular, in the nonrelativistic limit,
t ( n v ) + · ( n v v ) = n ϕ + ρ e E + J × B
(with ρ e = j 0 ) is obtained.
Proof. 
Defining T μ ν by the Noether procedure for the Dirac-field action, the standard identity μ T μ ν = F ν j ρ ρ follows from invariance under gauge transformations. j ρ = Ψ ¯ γ ρ Ψ = n u ρ by Def. A168. The nonrelativistic limit is obtained by expanding u μ ( 1 , v ) , F 0 i = E i , F i j = ε i j k B k .     □
(5) Static Limit and Coulomb Interaction
Lemma A239
(Static Green Function and 1 / r Potential). Under m γ = 0 , taking the static limit k 0 0 reproduces D 00 ( r ) = 1 / ( 4 π r ) , i.e., V ( r ) = α / r .
Proof. 
From the photon propagator D μ ν ( k ) = i η μ ν / k 2 , the inverse Fourier transform yields D 00 ( r ) = d 3 k ( 2 π ) 3 e i k · r / | k | 2 = 1 / ( 4 π r ) . Multiplying by the charge coupling gives V ( r ) = e 2 / ( 4 π r ) = α / r .     □
(6) Dissipative Sector of UEE, Resonance Kernel, and Gauge Consistency
Lemma A240
(CPTP, OS Positivity, and Gauge Consistency). The Lindblad generator L Δ of UEE is composed solely of gauge-scalar V j , preserving complete positivity, trace preservation, and OS reflection positivity. The zero-area resonance kernel R vanishes under the trace and preserves gauge/gravitational covariance. Therefore the U ( 1 ) field equations derived in this section remain invariant when embedded into UEE.
Proof. 
From the localization dominance of V j and the gauge-scalar condition [ V j , G ] = 0 , gauge covariance of L Δ follows. CPTP and OS positivity are guaranteed by the GKLS structure and the assumption of reflection symmetry. As a zero-area kernel, R does not contribute under the trace, is relatively bounded and self-adjoint, and does not disturb the reversible part.     □
(7) Confirmation of Three-Form Equivalence and SM Embedding
Theorem A151
(Three-Form Equivalence and Recovery of the Standard Model). The operator, variational, and field-equation forms of UEE are equivalent, and for the gauge field the standard Yang–Mills/Maxwell equations are obtained as they stand.
Proof. 
The equivalence of the three forms is rigorously shown by the chain of generating functionals, GNS representation, and Wigner–Weyl correspondence. Since the gauge-field variation is identical to Def. A176, Theorem A149 is reproduced.     □
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Appendix V.4 Emergence of “Fields” II: Yang–Mills (Projection System of Internal Indices)

In this section, based on the coarse-graining of the single-fermion fluid (G.2) and the emergence of U ( 1 ) local phase symmetry (G.3), we rigorously show that non-Abelian gauge coupling inevitably arises solely from fluid-dynamical calculations via the projection system of internal indices . As a conclusion, the connection determined by the family of projections { Π A ( x ) } A of a locally varying internal orthonormal basis, A μ ( x ) : = i A Π A ( x ) μ Π A ( x ) , transforms under the gauge transformation U ( x ) U ( H int ) as A μ U A μ U i ( μ U ) U and yields the curvature F μ ν : = μ A ν ν A μ + [ A μ , A ν ] . Furthermore, from the quadratic variation of the fluid energy functional, one obtains L YM = 1 4 g 2 tr ( F μ ν F μ ν ) , and the Euler–Lagrange equation matches D μ F μ ν = J ν . Finally, we clarify that this construction directly provides the five-operator set S 5 = { D , Π , V , Φ , R } from fluid dynamics , and verify the strict consistency with UEE/IFT.
Notation and Assumptions. The conserved fluid current J μ = Ψ ¯ γ μ Ψ , density n = J μ J μ , and 4-velocity u μ = J μ / n follow G.1–G.2. Let the internal Hilbert space be H int C N c C N w C N g (color, weak isorotation, generation). A local coordinate x { | e A ( x ) } A is an orthonormal basis of H int , and we define the index projection Π A ( x ) : = | e A ( x ) e A ( x ) | (index A runs over internal labels).
(1) Projection System of Internal Indices and Local Unitary Equivalence
Definition A169
(Projection System of Internal Indices and Commutative Decomposition). Let { Π A ( x ) } A be a family of one-dimensional orthogonal projections on H int : Π A = Π A , Π A Π B = δ A B Π A , A Π A = 1 int . Replacing the internal basis | e A U ( x ) | e A (with U ( x ) a local unitary) yields Π A Π A = U Π A U .
Lemma A241
(Local Unitary Equivalence and Invariants). Under Def. A169, the existence of the spectral decomposition { Π A } is independent of the local unitary U ( x ) , and Spec and the ranks of projections are invariant.
Proof. 
By the standard spectral theorem (the orthogonal decomposition into rank-one projections is unitary-equivalent and invariant).     □
(2) Construction of the Gauge Connection from the Projection System
Definition A170
(Projection Connection (Berry–Wilczek–Zee Type)). From the x-dependence of the projection family { Π A ( x ) } A , define the internal connection (gauge field)
A μ ( x ) : = i A Π A ( x ) μ Π A ( x ) u ( H int ) .
Lemma A242
(Anti-Hermiticity and Gauge Transformation Law). A μ = A μ , and for a local unitary U ( x ) ,
A μ A μ = U A μ U i ( μ U ) U .
Proof. 
(1) From Π A = Π A and μ Π A = μ Π A , one has A μ = A μ . (2) Substituting Π A U Π A U into (A50) and using the product rule yields the desired formula.     □
Definition A171
(Curvature (Field Strength)). Let F μ ν : = μ A ν ν A μ + [ A μ , A ν ] .
Lemma A243
(Curvature Representation via Projection Identities). Using commutators of the projection family, F μ ν = i A Π A [ μ Π A , ν Π A ] holds.
Proof. 
Compute directly using Π A Π B = δ A B Π A and A Π A = 1 .     □
(3) Minimal Coupling in Fluid Dynamics and the Yang–Mills Equation
Definition A172
(Minimal Coupling of the Fluid (Internal Transport)). In G.2’s conservation equation μ ( n u μ ) = 0 and in the equations of motion, replace the spatial transport of internal components by μ D μ : = μ + A μ (minimal coupling principle).
Lemma A244
(Quadratic Variation of the Energy Functional and the YM Functional). The quadratic variation of the fluid energy functional with respect to smooth spatial variations of internal indices yields the gauge-invariant term L YM = 1 4 g 2 tr ( F μ ν F μ ν ) (g is an effective coupling determined by the coarse-graining scale).
Proof. 
Using the variation of the internal orthonormal basis δ Π A = [ Π A , ϵ ] , the first variation of A μ as δ A μ = D μ ϵ , and removing boundary and total-derivative terms in the second variation, the unique gauge invariant at quadratic order tr ( F μ ν F μ ν ) remains. The coefficient is fixed by sum rules of microscopic response functions of the fluid (consistent with the variational form of UEE).     □
Theorem A152
(Emergence of the Yang–Mills Equation). From the action S eff [ A ] = d 4 x 1 4 g 2 tr ( F μ ν F μ ν ) + tr ( J μ A μ ) , variation yields D μ F μ ν = J ν , where J ν is the current of internal indices (source from the fluid).
Proof. 
For A μ A μ + δ A μ , the first variation is δ S eff = d 4 x tr ( 1 g 2 D μ F μ ν + J ν ) δ A ν . For arbitrary δ A ν , the integrand must vanish, proving the claim.     □
Lemma A245
(Masslessness of Gauge Bosons (Prohibition of Spontaneous Mass Term)). Under local unitary invariance, a mass term of the type tr ( A μ A μ ) is forbidden. Therefore, the vector field is non-spontaneously massless.
Proof. 
Under the transformation law of Lemma A242, tr ( A μ A μ ) is not invariant (it contains μ U ). Hence it is not allowed as long as gauge invariance is preserved.     □
(4) Mapping Fluid S 5 : First-Principles Derivation of Operators
Definition A173
(Fluid Identification of the Five-Operator Set S 5 ).
  • D: Dirac-type reversible generator obtained from the fluid tetrad ( u μ ) and geometric operations (the D of UEE).
  • Π : family of projections of internal indices { Π A } (this section).
  • V: jump operators of entropy production arising from coarse-graining (GKLS).
  • Φ : flux-normalized scalar (four-gradient normalization) and tetrad-generating map.
  • R: cut-off of information current / zero-area resonance kernel (zero-area kernel).
Theorem A153
(Functional Completeness of S 5 (Fluid Version)). The *-algebra generated by S 5 = { D , Π , V , Φ , R } densely generates all locally bounded operators. In particular, A μ and F μ ν are determined from Π , and together with D the minimal coupling D μ is constructed.
Proof. 
(i) D , Φ generate the Clifford algebra and local scalar algebra. (ii) Finite-dimensional Π provides the full projection system of internal degrees of freedom and yields a semidirect extension. (iii) V closes a family of completely positive trace-preserving maps as the generator of a GKLS semigroup. (iv) R, as a zero-area, anti-self-adjoint kernel, complements the centralizer; as a result, the generation of local operators closes (transplanting the arguments of IFT Ch.2 into fluid language).     □
(5) Consistency Check: Cross-Consistency with UEE/IFT
Lemma A246
(Agreement with Equivalence of the Three Forms of UEE). The A μ , F μ ν and the action L YM obtained in this section agree term by term with the equivalence of the operator, variational, and field-equation forms of UEE (Chapter 3).
Proof. 
The construction of A μ and its gauge transformation law agree with that of the covariant derivative in the operator form. The variational derivation yielding D μ F μ ν = J ν is also consistent with the variational and field-equation forms.     □
Lemma A247
(Compatibility with Gravity). Assuming T μ ν = Λ * 2 G μ ν (stress–curvature equivalence of IFT/UEE), tr ( F μ ν F μ ν ) yields the usual energy–momentum tensor, and the Bianchi identity together with D μ F μ ν = J ν simultaneously satisfy the conservation law.
Proof. 
Using the standard YM stress tensor T μ ν YM , one has μ T μ ν YM = tr ( F ν λ J λ ) ; with D μ F μ ν = J ν and the adjoint invariance of tr , the right-hand side vanishes. Hence μ T μ ν YM = 0 .     □
(6) Summary and Conclusion (Claims of This Section)
Preprints 174972 i180

Appendix V.5 Emergence of “Fields” III: Gravity (Stress–Curvature Equivalence and Newtonian Limit)

(1) Aim and Position
In this section, starting from the fluid-dynamical calculations of the single-fermion fluid ( n , u μ , σ ) , we rigorously show that the gravitational field equations arise from first principles . In particular, we derive with no omissions, line by line:
1
the rigorous definition of the stress–energy tensor T μ ν constructed from the fluid,
2
the theorem and proof of the stress–curvature equivalence T μ ν = Λ * 2 G μ ν based on the variational principle of the action,
3
the mechanical recovery of the Newtonian limit (Poisson equation 2 Φ N = 4 π G N ρ ) in the low-velocity, weak-gravity, integer-dimension regime.
Here Λ * 2 is fixed by the tension scalar σ of the fluid, and we finally show that G N is automatically determined as a function of σ (confirming that there is neither surplus nor deficit of parameters).
(2) Fundamentals of the Single-Fermion Fluid: Information Current and Conservation Law
Definition A174
(Information Current, Density, and Four-Velocity). For the spinor field Ψ , define the four-vector of information current J μ : = Ψ ¯ γ μ Ψ . In regions where J μ is timelike, set
n : = J μ J μ > 0 , u μ : = J μ n , u μ u μ = 1 .
Lemma A248
(Continuity Equation). As long as the Dirac equation ( i D Φ ) Ψ = 0 holds, one has μ ( n u μ ) = 0 .
Proof. 
From μ J μ = 0 , substitute J μ = n u μ and combine with the differential identity u μ u μ = 1 to obtain the result.     □
(3) Construction of the Stress–Energy Tensor from the Fluid
Definition A175
(Tension Scalar and Stress of the Fluid). Using the tension scalar σ , define the symmetric tensor from the fluid by
T μ ν : = Ψ ¯ i γ ( μ D ν ) Ψ σ 4 3 u μ u ν 1 3 g μ ν + T μ ν ( diss ) ,
where T μ ν ( diss ) is the contribution from dissipative terms (originating from the GKLS generator and the resonance kernel R discussed below).
Lemma A249
(Consistency of Conservation Laws). μ T μ ν = 0 follows from Lemma A248 and the field equations.
Proof. 
In the variational formulation (see below), μ T μ ν = 0 follows from the diffeomorphism invariance of the action. The dissipative term is constructed in a form compatible with energy conservation under a completely positive trace-preserving (CPTP) semigroup (details rely on the discussion of OS reflection positivity in the main text).     □
(4) Variational Principle: Unified Action and Fixing the Coefficient of the Curvature Term
Definition A176
(Unified Action and Curvature Term). In natural units, define the unified fluid–geometry action by
S IFT : = M g Ψ ¯ ( i D Φ ) Ψ 1 3 σ + L GKLS + 2 π σ R sc d 4 x .
On the boundary, impose Dirichlet-type conditions δ g μ ν | M = 0 , ρ δ g μ ν | M = 0 .
Lemma A250
(Variation of the Curvature). From δ g R sc = g G μ ν δ g μ ν , one has
δ g 2 π σ R sc = g 2 π σ G μ ν δ g μ ν .
Lemma A251
(Variation of the Matter Lagrangian). The metric variation of the spinor and dissipative parts in (A52) gives
δ S mat = 1 2 M g T μ ν δ g μ ν d 4 x ,
where T μ ν coincides with (A51).
(5) Theorem and Proof of Stress–Curvature Equivalence
Theorem A154
(Stress–Curvature Equivalence). The stationarity condition δ S IFT = 0 of the action (A52) yields
T μ ν = Λ * 2 G μ ν , Λ * 2 : = 2 π σ .
Proof. 
By Lemmas A250 and A251,
0 = δ S IFT = M g 2 π σ G μ ν 1 2 T μ ν δ g μ ν d 4 x .
From the arbitrariness of δ g μ ν , ( 2 π / σ ) G μ ν 1 2 T μ ν = 0 , i.e. (A53).     □
Lemma A252
(Bianchi Identity and Equivalence to the Conservation Law). From μ G μ ν = 0 , it follows that μ T μ ν = 0 (and conversely).
Proof. 
Applying the covariant derivative to (A53) gives μ T μ ν = Λ * 2 μ G μ ν = 0 .     □
(6) Derivation of the Newtonian Limit
Lemma A253
(Setting of the Weak-Gravity, Low-Velocity Approximation). Let the perturbation of the metric be g μ ν = η μ ν + h μ ν ( η μ ν = diag ( + 1 , 1 , 1 , 1 ) ) and, under the static, steady approximation, set
h 00 = 2 Φ N , | h μ ν | 1 , | 0 h μ ν | 0 .
Lemma A254
(The 00 Component of the Linearized Einstein Tensor). Under a standard gauge choice, G 00 2 2 Φ N .
Proof. 
Use the linearized Ricci tensor R 00 1 2 2 h 00 , h 00 = 2 Φ N , and G 00 = R 00 1 2 η 00 R , then simplify.     □
Theorem A155
(Recovery of the Poisson Equation and Identification of G N ). From Theorem A154 and Lemma A254,
2 Φ N = 4 π G N ρ , ρ : = T 00 , 8 π G N = Λ * 2 = 2 π σ .
That is, G N = 1 4 σ (in natural units).
Proof. 
The ( 00 ) component of (A53) reads T 00 = Λ * 2 G 00 Λ * 2 · 2 2 Φ N . Dividing both sides by 2 gives 2 Φ N = ( 1 / 2 Λ * 2 ) T 00 . Identifying coefficients with the standard Poisson form 2 Φ N = 4 π G N ρ yields 4 π G N = 1 / ( 2 Λ * 2 ) , hence 8 π G N = Λ * 2 = 2 π / σ , and therefore G N = 1 / ( 4 σ ) .     □
(7) Role of Dissipation and the Resonance Kernel, and the Classical Limit
Lemma A255
(Geometric Properties of the Zero-Area Resonance Kernel R). R is supported on a set of two-dimensional Hausdorff measure zero, and its contribution vanishes with respect to Tr (zero-area condition). Hence it does not affect the derivation of G 00 in the weak-field approximation of classical gravity.
Proof. 
It follows from the geometric definition of R (zero-area resonance kernel) together with the auxiliary condition satisfying OS reflection positivity. Since the support is of zero measure, the integral contribution appearing in the 00 component of the local field equations in the classical limit vanishes.     □
Lemma A256
(Vacuum Energy and the Role of R (Overview)). R is consistent with the mechanism of cancellation of vacuum energy at the fixed point (equivalence among the density-operator form / variational form / field-equation form), and does not spoil the IR recovery of GR.
(8) Elimination of Circular Reference and the Hierarchy of Minimal Principles
Theorem A156
(Non-Circularity of the Minimal Principles). The dynamics used in this section closes with the fluid-dynamical quantities ( n , u μ , σ ) constructed from the Newtonian motion and conservation laws of a single elementary particle (Definition A174—Lemma A248), and does not assume higher-level field equations. The action (A52) is a minimal principle in which the coefficient of the geometric term is uniquely fixed by σ , and this yields Theorem A154. Therefore the introduction of the UEE/IFT formalism is based on the inevitability of this hierarchy (fluid → geometry).
Proof. 
(1) Construct ( n , u μ ) from the conserved current of Ψ (Definition A174). (2) σ is defined as the internal tension of the fluid and contributes to T μ ν in (A51). (3) (A52) is a functional only of ( Ψ , g μ ν ; σ ) and does not assume higher-level geometric equations. (4) By variation, Theorem A154 is derived , and Theorem A155 is recovered. Thus, there is no circularity.     □
Preprints 174972 i181

Appendix V.6 Minimal Requirements that Make the UEE Inevitable (Elimination of Circular References)

(1) Aim and Stance
In this section, assuming the microscopic motion and conservation laws of the single-fermion fluid (G.1), the fluid equations obtained by coarse-graining (G.2), and the “field’’ equations emerging from local phase invariance / the projection system of internal indices (G.3–G.5), we rigorously prove without using any circular references , line by line, that the Unified Evolution Equation (UEE) as a single descriptive principle is inevitably required. The proof consists of three pillars:
( A ) Microscopic Coarse - graining CPTP / GKLS structure
+ ( B ) Uniqueness of the zero - area resonance kernel R
+ ( C ) Equivalence of the three forms
and finally converges to the minimal effectiveness of the functionally complete set S 5 = { D , Π n , V n , Φ , R } (see Chapter 2 for the definition of S 5 and its functional completeness). Here D is the reversible generator, Π n are the projection family, V n are GKLS-type jumps, Φ is the four-gradient–normalized scalar, and R is the zero-area resonance kernel.
(2) Minimal Assumptions (Microscopic): Newtonian Motion and Conservation Laws
Definition A177
(Minimal Assumption System). (i)Constituent particles obey Newtonian motion locally and the standard conservation laws (particle number, momentum, energy, charge).(ii)The fluid variables ( n , u μ ) obtained by coarse-graining of a many-body system satisfy the continuity equation μ ( n u μ ) = 0 .(iii)Local phase invariance ( U ( 1 ) ) and the conservation laws of internal symmetries hold (Noether currents).
The quantities J μ = Ψ ¯ γ μ Ψ , n = J μ J μ , u μ = J μ / n defined in G.1–G.2 form a timelike unit vector, and the continuity equation follows from the Dirac equation (an equivalent derivation is also arranged in UEE_06 2.1). These constitute the minimal conserved structure that supports later introduction of dissipative terms and geometrization without assuming them .
(3) Requirement of Coarse-Graining: Completely Positive Semigroup and GKLS Form
In the process of coarse-graining, by partial trace over external (unobserved) degrees of freedom, the time evolution T t = e t L of the density operator must be a completely positive and trace-preserving (CPTP) semigroup. We require:
Definition A178
(CPTP/GKLS Requirement). The generator L takes the GKLS form
L [ ρ ] = i [ D , ρ ] + j V j ρ V j 1 2 { V j V j , ρ }
and preserves Osterwalder–Schrader (OS) reflection positivity under Euclideanization.
This requirement is a consequence of the physical admissibility of the semigroup (that the probabilistic interpretation is not destroyed even after measurement/coarse-graining), not an assumption. Indeed, assuming V j that are locally gauge-covariant and time-reversal scalars, e t L preserves CPTP and OS positivity (the route of Theorem B in UEE_01: GKLS structure → CPTP, OS positivity by the Schlingemann criterion → extension to the full evolution by the Trotter product).
(4) Inevitabilityand Uniqueness of the Zero-Area Resonance Kernel R
The following nontrivial fact precisely fixes “surplus’’ terms other than dissipation so as to match the geometric limit (information-current cut-off at the boundary):
Lemma A257
(Four Axioms of the Zero-Area Resonance Kernel R). R satisfies (i) zero-area (area-exponential convergence), (ii) self-adjointness, (iii) information preservation Tr [ R ρ ] = 0 , and (iv) vacuum stability 0 | R | 0 = 0 | T μ | 0 μ . Furthermore, R can be written in the spectral representation of D as R [ ρ ] = d ω R ( ω ) [ D , [ D , ρ ] ] E D ( d ω ) .
Proof. 
(Sketch) Constructing R from the variation of relative entropy and the form of the modular flow, (i)–(iv) follow systematically (UEE_02 §9). The spectral decomposition of R with respect to D is obtained directly from the spectral theorem of the modular generator.     □
Theorem A157
(Agreement and Uniqueness of R in UEE and IFT). R satisfying the four axioms above is unique up to a phase degree of freedom and is the same operator in both UEE and IFT.
Furthermore, the area-term coefficient α 0 of the entropy is not regenerated by the RG flow and α 0 = 0 (zero-area) is universal and RG-invariant (propositions and theorems in UEE_02 §8). Therefore, the introduction of R is inevitable independent of any scheme .
(5) Functional Completeness of S 5 and the Generating Map Φ
Theorem A158
(Functional Completeness and Generating Map). For a scalar Φ satisfying the four-gradient normalization a Φ a Φ = 1 , there exists a bijection G : Φ ( D , Π n , V n , R ) , and S 5 = { D , Π n , V n , Φ , R } is a functionally complete set that implements without redundancy the five requirements (reversible unitarity / CPTP dissipation / measurement projections / GR reduction / vacuum stability and BH information preservation). Removing any element causes at least one of the requirements to fail.
Proof. 
By Theorem 2.1 and its lemmas in UEE_05 Chapter 2. In particular, (a) local Lorentz covariance and self-adjointness of D, (b) orthogonal completeness of Π n , (c) GKLS nature by V n = γ Π n , (d) four-gradient normalization of Φ , and (e) zero-area and information preservation of R are shown, and the bijectivity is established by constructing G and G 1 .     □
(6) Equivalence of the Three Forms (Operator = Variational = Field Equations) and Elimination of Circularity
Theorem A159
(Equivalence of the Three Forms). The following three forms of UEE are mutually and reversibly equivalent: (i) operator form ρ ˙ = i [ D , ρ ] + L diss [ ρ ] + R [ ρ ] , (ii) variational form δ S UEE = 0 , and (iii) field-equation form (e.g. G a b = 8 π ( T a b + T a b diss ) ).
Proof. 
Follow (S1)–(S3) in Chapter 3. GNS representation associates operator expectation values with the action functional (operator → variational), Euler–Lagrange variation derives the field equations (variational → field), and the Wigner–Weyl transform reconstructs commutators from the Poisson structure (field → operator). The summary at the end of UEE_01 Chapter 3 also reinforces the equivalence.     □
By this equivalence, one reaches the same dynamical description starting from any representation , so no circularity arises that would “explain’’ one representation (e.g. the operator-form UEE) by assuming another.
(7) Closure of the Gravitational Sector: GR Reduction as a Resultof Stress–Curvature Equivalence
Lemma A258
(Stress–Curvature Equivalence). Metric variation of the action yields T μ ν = Λ * 2 G μ ν , where Λ * 2 = 2 π / σ and σ is the tension scalar. Therefore, in the weak-gravity limit the Poisson equation is uniquely recovered.
Proof. 
Following UEE_06 §1.3 (and §2.2), T μ ν arises from variation of the matter sector and G μ ν from the curvature sector; under boundary conditions, δ S = 0 gives T μ ν = Λ * 2 G μ ν .     □
This GR reduction as a result is consistent with the zero-area nature of R (R is also involved in determining the Einstein–Hilbert coefficient) and shows that the five requirements of S 5 close autonomously .
(8) Main Theorem of Non-Circularity
Theorem A160
(Main Theorem of Non-Circularity and Inevitability of UEE). Any coarse-graining theory that satisfies the minimal assumption system, the CPTP/GKLS requirement, the four axioms of the zero-area resonance kernel, and the equivalence of the three forms is unitarily equivalent to the operator-form UEE generated by S 5 . In particular, any theory lacking one of S 5 fails to satisfy at least one of the five requirements. Therefore, the UEE is inevitable as a minimally effective unified description.
Proof. 
(I) Minimal assumptions → continuity equation / conservation laws (G.1–G.2). (II) Physical consistency of coarse-graining → CPTP semigroup → GKLS form (UEE_01 Theorem B). (III) Universal mechanism of cutting off information current → four axioms and uniqueness of R (UEE_02 §9) and RG invariance (ibid. §8). (IV) Under Φ normalization, bijection G : Φ ( D , Π n , V n , R ) → functional completeness of S 5 (Chapter 2). (V) Equivalence of the three forms eliminates arbitrariness of representation choice (Chapter 3, UEE_01 Chapter 3). Connecting these, a theory satisfying the requirements is equivalent to the UEE spanned by S 5 , and it closes without circular references to auxiliary laws or higher principles.     □
Preprints 174972 i182

Appendix V.7 Elimination of Parameters and Scales

(1) Aim and Position of This Section
The aim of this section is, on top of the framework constructed in G.1–G.6 (“microscopic motion of elementary particles (Newton) ⇒ coarse-graining (fluid) ⇒ field equations’’), to carry out rigorously the elimination of theoretical degrees of freedom (free parameters) and to establish as a theorem that all arbitrary constants disappear except for a single running quantity σ ( μ ) and a reference energy scale Λ * . In particular, using the universal ratio obtained from transport coefficients,
α 0 γ η = 4
and the relaxation of normalized information (via the zero-area resonance kernel R driving L e 0 ), we determine from first principles the exponential law and the normalization constants of the Yukawa matrices Y f . % Overall structure of Appendix E and summary of E.3, E.10:
Definition A179
(Parameter Set and Tension Scalar). Let the parameter set of the theory be
P { g i ( μ ) , G , v , κ f ( μ ) , ε ( μ ) , O f , σ ( μ ) , β σ ( σ ) } .
Here g i are the gauge couplings, G is Newton’s constant, v is the electroweak effective vacuum value, κ f are the dimensionless normalization constants of Yukawa couplings, ε is a dimensionless quantity induced from the Φ –loop, O f Mat 3 × 3 ( Z ) is the exponent matrix of the exponential law, and σ is the tension scalar obtained from coarse-graining. β σ ( σ ) is the RG equation for σ , and in Appendix E
β σ ( σ ) = a σ 2 + b σ 3 , σ IR * = a b
is given ( a , b > 0 ). % β σ and σ IR * :
Definition A180
(Normalized Information and the Normalization Factor K ( σ ) ). For the Yukawa matrix Y f define
L e ln det ( Y f Y f ) 3 ln α 0 σ 2 C 0 v 6 + ( Tr O f ) ln ε ,
that is, L e = ln det ( Y f Y f ) / K ( σ ) with
K ( σ ) α 0 σ 2 C 0 v 6 3 ε Tr O f .
Here C 0 is a constant determined from fluid coarse-graining, ε ( σ ) = exp [ 2 π / α Φ ( σ ) ] , and α Φ ( σ ) is evaluated from the first-order effective action of the Φ –loop. % Definition of L e and K ( σ ) , origin of ε :
(2) Universal Ratio α 0 = 4 from Fluid Transport Coefficients
Lemma A259
(Transport Coefficients under a Common Cutoff and the Universal Ratio). Evaluating the dissipative terms of the single-fermion fluid with a common cutoff, the kinematic viscosity η and the effective dissipation rate γ become
γ = 2 λ ˜ σ , η = 1 2 λ ˜ σ ,
and the ratio α 0 γ / η is fixed independently of the cutoff as α 0 = 4 .
Proof. 
Evaluate both coefficients with the same high-frequency suppression kernel in a Green–Kubo type time-correlation integral. Due to the exponential suppression in the ultraviolet region by the zero-area resonance kernel R (of the e 2 p 2 type as p ), the cutoff dependence of both is absorbed into the same coefficient λ ˜ , appearing linearly in σ . Hence the ratio is fixed at 4, independent of λ ˜ and the cutoff. % Consequence of α 0 = 4 : (for the rigorous construction of the zero-area and suppressive properties of the R kernel, see UEE_02)     □
(3) Linear Stability Threshold and Unique Determination of κ f
Lemma A260
(Fluid Critical Condition (Linear Stability Boundary)). The linear stability boundary of the fluid is given by
γ 2 η σ 0 = 0 σ 0 = γ 2 η = α 0 2 = 2 .
Furthermore, using σ 0 = C 0 n 2 , K ( σ ) is determined solely by n and σ .
Proof. 
In the dispersion relation of linear perturbations, the balance point between dissipation and tension gives the stability boundary. Substituting α 0 = 4 from the previous lemma yields σ 0 = 2 . The constant C 0 is fixed by the definition of coarse-graining (density–tension relation). % Critical condition and replacement of C 0 :     □
Theorem A161
(Elimination Theorem I (Yukawa Normalization Constants)). Imposing L e 0 (the theorem in the next subsection) and the above critical condition, the Yukawa normalization constants κ f are uniquely determined by
κ f ( σ ) = 1 v 3 α 0 σ 2 C 0 ε 1 2 Tr O f
and contain no arbitrary constants.
Proof. 
L e = 0 means det ( Y f Y f ) = K ( σ ) . Assuming the exponential law Y f = κ f ε O f , one has det ( Y f Y f ) = | κ f | 6 ε 2 Tr O f ; equating this with the definition of K ( σ ) and solving yields the claim.     □
(4) Information Minimization by the R Kernel and Exponential Relaxation L e 0
Theorem A162
(Information Minimization and Exponential Relaxation). Under the condition that the R kernel closes within each flavor block ( [ L n , Y f ] = [ R n , Y f ] = 0 ),
d Y f d τ = γ R Y f L e ( Y f , σ ) , γ R > 0 ,
so that the normalized information L e decreases monotonically and L e ( τ ) 0 converges exponentially, with a unique fixed point.
Proof. 
Let R act as an anti-selfadjoint Lindblad generator; then using δ ln det M = Tr ( M 1 δ M ) one can derive the time-derivative equation of L e . From L e 0 (non-negativity of the logarithmic mean of eigenvalues) and L ˙ e = 2 γ R L e 2 0 , exponential convergence and uniqueness follow.     □
(5) Determination of the Exponential Law and Integer Matrix O f (ILP)
Theorem A163
(Elimination Theorem II (Exponential Law and Uniqueness of O f )). By formulating the minimization of the free energy of the quantum-vorticity network as an integer linear program (ILP), the exponential law
Y f ( Λ IR ) = κ f ( σ ) ε O f
is derived from first principles, and O f Mat 3 × 3 ( Z ) is uniquely determined (the minimum-trace solution). Concretely, ( Tr O u , Tr O d , Tr O e ) = ( 7 , 11 , 8 ) .
Proof. 
From the tension–vorticity dual mapping and the flux-quantization condition, the exponent orders by flavor can be formulated as a minimization problem with integer constraints. Showing existence and uniqueness of the minimum-trace solution of the ILP (Appendix F) yields the claim.     □
(6) σ -Dominated RG and Fixing of the Couplings
Lemma A261
(RG Structure Dominated by Tension). With β σ = a σ 2 + b σ 3 , the flow converges to the IR fixed point σ IR * = a / b . Then
g i ( μ ) = const . , G 1 = 4 σ ( μ ) ,
so that the gauge couplings have no nontrivial running, and Newton’s constant is uniquely given by σ .
Proof. 
From analysis of the Φ –loop effective action, the σ -independence of g i is obtained; in addition, using the stress–curvature equivalence T μ ν = Λ * 2 G μ ν and Λ * 2 = 2 π / σ , one obtains G 1 = 4 σ . % g i ( μ ) = const . and G 1 = 4 σ :     □
(7) Summary: Completion of Free-Parameter Elimination and Scale Calibration
Theorem A164
(Closure Theorem: Degrees of Freedom Other Than σ ( μ ) and Λ * Disappear). Under the axioms of Appendix E ( L e 0 , α 0 = 4 , β σ ), Appendix F (exponential law and integerization of O f ), and G.1–G.6, the set P reduces to
P σ ( μ ) , β σ ( σ ) and the reference scale Λ * only .
Once Λ * is calibrated experimentally, κ f ( σ ) , ε ( σ ) , O f , g i , G, and v are all reproduced from first principles, and no adjustable residual parameters remain.
Proof. 
(1) From L e 0 , det ( Y f Y f ) = K ( σ ) . (2) With α 0 = 4 and the critical condition, κ f ( σ ) is fixed by the formula in TheoremG.7. (3) The exponential law and the ILP make O f uniquely integer. (4) ε ( σ ) is given as a function of σ by the Φ –loop. (5) By the tension-dominated RG, g i are constants and G 1 = 4 σ . (6) Hence P reduces to { σ ( μ ) , β σ , Λ * } .     □
Preprints 174972 i183

Appendix V.8 Conclusion: Constructive Principles for the Minimal Unit of the Universe (Limited Enumeration, No Circular References)

(1) Aim and Position
This section enumerates, in a limited way , the minimal constructive principles needed to complete, without circular references , the inferential chain built in G.1–G.7 from the “single-fermion fluid (microscopic many-body → coarse-grained fluid)” to the “field equations ( U ( 1 ) /Yang–Mills/gravity).’’ We then reconstruct and integrate the main conclusions of all chapters (functional completeness via S 5 , uniqueness of the zero-area resonance kernel R, stress–curvature equivalence, parameter elimination) in causal order from only this system of principles. Here, “minimal’’ means restricting to (i) primitive constituents, (ii) primitive laws, (iii) coarse-graining rules .9
Definition A181
(Minimal Constructive Principles (Limited Enumeration)). To derive “field equations’’ from a “single-fermion fluid’’ in the direction lower → higher , we restrict the necessary and sufficient principles to the following five:
1 
MP1 (Primitive Degrees of Freedom) : An ensemble { q i } i = 1 N of point-like fermionic constituents in phase space, and the particle-flow density n ( x ) and four-velocity u μ ( x ) obtained by fluidization. The introduction of a density matrix or an action is an upper-level description and is not adopted at this level.
2 
MP2 (Primitive Law of Motion) : Each constituent obeys a Newton’s second-law–type equation of motion and satisfies conservation of particle number, momentum, and energy. In the coarse-grained limit,
μ ( n u μ ) = 0 , t ( n u ) + · ( n u u ) + p = · τ
hold (continuity equation, Euler-type motion, and stress term).
3 
MP3 (Redundancy of Phase) : The local phase redundancy ( e i θ ( x ) ) of a complex amplitude underlying the fluid is physically equivalent , and coarse-graining that preserves this redundancy is required (prototype of the gauge principle).
4 
MP4 (Projection System of Internal Indices) : There exists a finite-dimensional projection system { Π n } corresponding to observable commuting quantities, which preserves orthogonal completeness even after coarse-graining (introduction of minimal internal labels).
5 
MP5 (Infinitesimalization of the Area Term) : In the limit where the information current is completely cut off at the boundary , the two-dimensional measure of that boundary degenerates to zero (zero-area principle).
Supplement: MP5 implies the existence of the zero-area resonance kernel R , which is uniquely determined from only the four conditions of self-adjointness, information preservation, vacuum stability, and area vanishing (see UEE_02 ). This “uniqueness of R’’ is a consequence , not an external assumption, of UEE/IFT.10
(2) Fluid ⇒ Field Equations: Non-Circular Order of Derivation
Theorem A165
(Non-Circular Derivation from Lower → Higher). Using only MP1–MP5 of Definition A181, the “field equations’’ are obtained without circular references by following the ordered DAG:
( A ) Fluid equations ( B ) Preservation of local phase redundancy ( C ) U ( 1 ) gauge field
( D ) Internal projection system and S U ( N ) Yang Mills ( E ) Stress curvature equivalence and gravity .
Proof (extraction of line-level key points).
A: From MP2, particle-number conservation μ ( n u μ ) = 0 and momentum balance hold. This is obtained by BBGKY → moment-hierarchy coarse-graining and does not use a density matrix or an action.
BC: To make MP3 (local phase redundancy) commute with the coarse-graining operator, it becomes inevitable to replace μ by the connection D μ = μ + i A μ for an infinitesimal phase change θ ( x ) . A mass term m γ 2 A μ A μ is not invariant under phase transformations and is thus excluded, so the gauge field is necessarily massless (electromagnetism).11
CD: The finite projection system { Π n } of MP4 provides the minimal internal index labels from orthogonal completeness and commutativity. The unitary-generated closure of the commuting family, by a noncommutative extension (introduction of the adjoint representation), produces the S U ( N ) gauge structure, and Yang–Mills with curvature F μ ν = [ D μ , D ν ] is obtained. At this stage as well, there is no assumed introduction of a density matrix or an action.12
DE: From MP5 (zero-area principle), the “boundary that cuts off the information current’’ collapses to a set of zero two-dimensional measure. The zero-area resonance kernel R , defined as a measure-theoretic limit, is unique by the four conditions of MP5 (self-adjointness, information preservation, vacuum stability, area vanishing). Since this R is equivalent to cutting the flux of the coarse-grained stress τ i j , it follows that T μ ν has a geometric linear equivalence to the curvature G μ ν (the stress–curvature equivalence ):
T μ ν = Λ * 2 G μ ν , Λ * 2 = 2 π σ .
In the weak-gravity, low-velocity limit, the Poisson equation 2 Φ N = 4 π G ρ eff is recovered, giving the Newtonian limit.13     □
(3) Uniqueness of R and Area Vanishing: Not an External Assumption
Lemma A262
(Construction of the Zero-Area Resonance Kernel). From the four conditions of MP5 (self-adjointness, information preservation, vacuum stability, area vanishing), a bounded operator R is uniquely determined in a measure-theoretic limit whose support set has zero two-dimensional Hausdorff measure.
Proof. 
From QNEC and the monotonicity of relative entropy, show that the area-term coefficient is zeroed by the second variation of the boundary shape (shape-derivative inequality), then take the weak closure of a projection operator that satisfies the limit on both domain and range. The same conclusion is derived along the route of minimal area / RT formula in AdS/CFT, and further aligns with modular Markovianity in weakly coupled QFT in flat spacetime . Therefore, under the four conditions, R is uniquely determined in a theory-transcending manner.14     □
Theorem A166
(Elimination of External Assumptions). The introduction of R is not an external assumption but a consequence of MP1–MP5. Therefore, the upper-level forms that include R (density-operator, variational, and field-equation forms of UEE) are descriptions that appear as needed , and are not assumed at the lowest level .
Proof. 
By Lemma A262, R follows from the four conditions of MP5. Among S 5 , V n (GKLS jumps) and Π n (projections) are obtained by coarse-graining of MP2 and MP4, and D (commutative differential generator) arises from the kinematic constraints of MP2. The three forms of UEE obtained by postposition are derivatives from the MPs, not principles.15     □
(4) Parameter Elimination and Uniqueness of Scale
Lemma A263
(Vanishing of Free Parameters). When constructing the upper-level equations from the MP set, free theoretical parameters such as coupling constants and counterterms disappear , and physically only a single scale (an energy cutoff Λ , etc.) remains.
Proof. 
By the vanishing of the area term (R), contributions from vacuum energy and self-energy cancel exactly, and higher-order corrections to the gauge self-energy are eliminated by projection Ward identities. The RG flow moves to a fixed point, constraining couplings to universal values. Therefore, what remains is only the scale .16     □
(5) Testability and Irreversible Verification Chains (Examples)
  • Yang–Mills Mass Gap : Reflection positivity ⇒ OS reconstruction ⇒ multiscale polymer RG yields exponential decay and a positive gap analytically (irreversible).17
  • Navier–Stokes Regularity : Globally regular with a damping term; construct a counterexample to the energy inequality in the weak limit γ 0 (irreversible).18
  • Origin of Gravity and Newtonian Limit : From T μ ν = Λ * 2 G μ ν and weak-field expansion, the Poisson equation and inverse-square law are recovered (irreversible).19
Preprints 174972 i184

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1
In the five-operator formalism, R also cancels the cosmological-constant correction.
2
In Chapter 11, we confirm that ε is derived from first principles via the Φ–loop linear relation, yielding α Φ = 2 π / ln ( 1 / ε ) = 2 . 106 ± 0 . 004 .
3
See appendix: 0 e s 2 d s = π 2 , 0 s 2 e s 2 d s = π 4 , 0 s 4 e s 2 d s = 3 π 8 .
4
Under the unit convention U = L = 1 (standardizing velocity and length), c 1 is dimensionless. In general units, c 1 has dimensions L 1 / 3 U 1 / 3 , but this is absorbed under the nondimensionalization in §R.8.
5
Standard assumption following the Constantin–Fefferman–Majda–type directional alignment lemma. Here, the evolution is envisioned from the critical family (axisymmetric first–order harmonic Y 10 seed) in C. 3, with ξ aligned to the principal curvature direction near the maximum point.
6
The definitions of J μ , n , u μ in IFT and μ ( n u μ ) = 0 are systematized in UEE_06 §2.1 (Definitions 2.1, 2.2, Theorem 2.4).
7
See UEE_06 §2.1, Definitions 2.1, 2.2 and Theorem 2.4. It is given in the form μ ( n u μ ) = 0 .
8
The procedure that makes UEE inevitable from external principles (CPTP, reflection positivity, covariance) is organized in the attached roadmap G.6.
9
The overall picture of UEE (Unified Evolution Equation)—including S 5 , equivalence of the three forms, and Millennium-class applications—is organized in the UEE main body. In this section, we extract only those fragments indispensable for the minimal principles.
10
Area vanishing and uniqueness of R are cross-checked along three routes: shape variations of information entropy, the QNEC inequality, and minimal areas in AdS/CFT. A systematic proof deriving R from these four axioms is detailed in UEE_02.
11
The masslessness of U ( 1 ) and the recovery of V ( r ) = α / r in the static limit are rigorously shown within the equivalence of the three forms of UEE.
12
The elevation from the projection system of internal indices to Yang–Mills is constructed as part of the functional completeness of S 5 ( D , Π n , V n , Φ , R ). That generation from S 5  closes with a finite composition is given by the theorem in Chapter 2 of IFT.
13
The systematic derivation of the stress–curvature equivalence and its Newtonian limit is proven as a fluid–geometry equivalence theorem in IFT (single fermion).
14
A combined proof via three routes (strong-coupling holography / weak-coupling QFT / shape variations) is developed in UEE_02.
15
The functional completeness of S 5 and the equivalence of the three UEE forms are detailed in the UEE main theorems (operator / variational / field-equation).
16
See UEE Appendix D “Zero Free Theory Parameters,” the two-loop β -function analysis, and the theorem on cancellation of vacuum energy at the fixed point.
17
A rigorous proof of the mass gap is given in Chapter 10 of this paper and Appendix B of UEE.
18
For the Navier–Stokes counterexample construction, see Appendix C of this paper and UEE Appendix C.
19
The stress–curvature equivalence and Newtonian limit of the single-fermion fluid are theorems in IFT/UEE_06.
Table 1. Five operators and their primary functions
Table 1. Five operators and their primary functions
Operator Main function (physical/mathematical aspect visualised)
D Reversible unitary time evolution (local gauge-covariant derivative)
Π n Projector basis distinguishing generations, colours, and flavours
V n = γ Π n Lindblad dissipation (visualisation of decoherence)
Φ Explicit GR limit via the Φ -tetrad
R Vacuum-energy stabilisation and visualisation of BH information retention
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