Relativistic Quantum Theory Extended to the Universe - the New Constant H_x and How it Contributes to the Sun’s Charge

1. Introduction

Relativity and quantum mechanics are successfully related in the work of Dirac [1]. From the point of view of relativistic quantum mechanics description and physical worldview, it is the weak gravitational field that can be successfully described. For the present paper, it is important to point out that, starting from the mathematical-physical foundations originally formulated by Dirac and later developed further, the possibility of quantization for weak gravitational fields has been demonstrated. One important and fundamental reference can be mentioned, which is attributed to Bronstein. His original paper [2] is one of the first to formulate a proven link between relativistic quantum mechanics and weak gravitational fields. This was successfully demonstrated by modern research.

The present paper focuses on the ‘now-classical’ Dirac formulation and continues it from a new physical point of view. It is very important to state now that the mathematical description of relativistic quantum mechanics established by Dirac does not have a distinguished scale. If we ask the question where a weak gravitational field exists, the answer is simple: the set of solar system-like systems, the stars, as we know them (in other words, the world as we know it, the Universe) is almost entirely characterised by a weak gravitational field. This justifies the question of whether it is possible to extend the physical-mathematical description of quantum mechanics to the Universe (nearly the whole of it, as defined by the weak gravitational field). This extension would be justified if we could apply to solar system-like systems a physical model where masses (stars, planets) could be considered as ‘mass points’ and also have a charge (and also be considered as indistinguishable mass points and have quantized orbits in solar system-like systems). The first two criteria are easily met, at least in thought. “Considered as mass points” is trivial, and “having charge” appears in many works. For other important aspects, see later in point 5. and 6.

2. Overview of Relativistic Quantum Mechanics and Gravitational Potential

The simplest way to describe the physical model of an atom with a single electron is to use the mathematical tools of quantum mechanics. Let’s start with this. Consider an e-charged particle of mass μ moving in a system with central mass M. Assume that the electromagnetic effects and the gravitational effects act independently of each other, simultaneously. The energy is the sum of the kinetic energy of the μ-mass particle and the potential energy (V):

$$\mathrm{H}={\displaystyle \frac{1}{2}}\mathrm{\mu }\left({\mathrm{v}}_{\mathrm{x}}^2+{\mathrm{v}}_{\mathrm{y}}^2+{\mathrm{v}}_{\mathrm{z}}^2\right)+\mathrm{V}\left(\mathrm{x},\mathrm{y},\mathrm{z}\right)$$

(1)

The energy operator can be written as:

$$\mathbf{H}=-{\displaystyle \frac{1}{2\mathrm{\mu }}}\left({\displaystyle \frac{{\partial }^2}{\partial {\mathrm{x}}^2}}+{\displaystyle \frac{{\partial }^2}{\partial {\mathrm{y}}^2}}+{\displaystyle \frac{{\partial }^2}{\partial {\mathrm{z}}^2}}\right)+\mathrm{V}\left(\mathrm{x},\mathrm{y},\mathrm{z}\right)$$

(2)

From the above equation, the Hamiltonian function:

$$\mathbf{H}={\displaystyle \frac{1}{2\mathrm{\mu }}}{\left(\underset{¯}{\mathrm{p}}-{\displaystyle \frac{\mathrm{e}}{\mathrm{c}}}\underset{¯}{\mathrm{A}}\right)}^2+\mathrm{U}$$

(3)

Assume that the centre of mass μ moves in the weak gravitational field of the central mass M. Here p is the momentum vector (the vector potential A is zero in our case. In the applicable gravitational equations, we assume a weak static gravitational field, the tensor component g_ik is time-independent, there is no energy flux, and there is a simple linear relation between g₄₄ and the potential energy). In special relativity, the energy-momentum tensor must lead to a solution such that, far from a static M mass point (here: star), it is equivalent to the Newtonian gravitational potential. The Newtonian gravitational potential is denoted U₂. Considering the above, the following Hamiltonian function can be written for weak gravitational fields. Here we differ from the usual quantum mechanical approach in the first time. The only deviation from the original approach is the equation U = eU₁+U₂:

$$\mathbf{H}=\mathrm{c}\sqrt{{\mathrm{\mu }}^2{\mathrm{c}}^2+{\mathbf{p}}^2}+\mathrm{e}{\mathrm{U}}_1+{\mathrm{U}}_2$$

(4)

where ${\mathrm{U}}_1={\mathrm{U}}_1(\mathrm{r})=-{\displaystyle \frac{\mathrm{e}}{\mathrm{r}}}$ the Coulomb potential, ${\mathrm{U}}_2=-{\displaystyle \frac{{\mathrm{f}}_{\mathrm{x}}\mathrm{M}\mathrm{\mu }}{\mathrm{r}}}$ the gravitational potential

In the following, we refer to derivations that are well known from the literature, while omitting the full details. (These derivations can also be found in [3].) The following are the steps of the derivation of the Dirac equation according to Bethe and Salpeter [4] p. 47-52. To carry out the square root in quantum mechanics, operators similar to the Pauli spin operators can be introduced. Following the linearization performed by Dirac:

$$\sqrt{{\mathbf{p}}_{\mathrm{x}}^2+{\mathbf{p}}_{\mathrm{y}}^2+{\mathbf{p}}_{\mathrm{z}}^2}={\mathbf{\sigma }}_{\mathrm{x}}{\mathbf{p}}_{\mathrm{x}}+{\mathbf{\sigma }}_{\mathrm{y}}{\mathbf{p}}_{\mathrm{y}}+{\mathbf{\sigma }}_{\mathrm{z}}{\mathbf{p}}_{\mathrm{z}}$$

(5)

For the above reasons, it can finally be written that:

$$\mathbf{H}=\mathrm{e}{\mathrm{U}}_1+{\mathrm{U}}_2+\mathrm{c}{\mathbf{\rho }}_1({\mathbf{\sigma }}_{\mathrm{x}}{\mathbf{p}}_{\mathrm{x}}+{\mathbf{\sigma }}_{\mathrm{y}}{\mathbf{p}}_{\mathrm{y}}+{\mathbf{\sigma }}_{\mathrm{z}}{\mathbf{p}}_{\mathrm{z}})+{\mathrm{\rho }}_3{\mathrm{\mu }}_0{\mathrm{c}}^2$$

(6)

The energy operator E:

$$\mathbf{E}=-{\displaystyle \frac{\hslash }{\mathrm{i}}}{\displaystyle \frac{\partial }{\partial \mathrm{t}}}$$

(7)

The equation of state using the known form of the energy operator:

$\mathbf{H}\mathrm{\psi }=\mathrm{E}\mathrm{\psi }$

which can be written as follows:

$${\displaystyle \frac{\hslash }{\mathrm{i}}}{\displaystyle \frac{\partial \mathrm{\Psi }}{\partial \mathrm{t}}}+\left[{\displaystyle \frac{\hslash \mathrm{c}}{\mathrm{i}}}{\mathrm{\rho }}_1\left({\mathbf{\sigma }}_{\mathrm{x}}{\displaystyle \frac{\partial }{\partial \mathrm{x}}}+{\mathbf{\sigma }}_{\mathrm{y}}{\displaystyle \frac{\partial }{\partial \mathrm{y}}}+{\mathbf{\sigma }}_{\mathrm{z}}{\displaystyle \frac{\partial }{\partial \mathrm{z}}}\right)+{\mathrm{\rho }}_3{\mathrm{\mu }}_0{\mathrm{c}}^2+\mathrm{U}\right]\mathrm{\Psi }=0$$

(8)

Formally, the equation above differs from the usual Dirac equation in the U₂ term, where $\mathrm{U}=\mathrm{e}{\mathrm{U}}_1+{\mathrm{U}}_2$. (The consequences of this difference are discussed in detail below). The rest of the solution is partly explained in [1].

3. Derivation of the Radial Part of the Relativistic Dirac Equation

The state function Ψ depends on the variables x, y, z, t, and the variables s=±1/2 and r==±1/2, so the state function can be written as follows:

Ψ = Ψ(x,y,z,t,r,s)      (9)

Expressed in terms of the eigenfunctions, we obtain the following (here we have assumed that spin and motion are independent, so the eigenfunctions can be separated into coordinate-dependent and spin-dependent parts, and the same is true for the eigenfunctions ξ, η acting on the r-degree of freedom):

$$\mathrm{\Psi }={\mathrm{\Psi }}_1\left(\mathrm{x},\mathrm{y},\mathrm{z},\mathrm{t}\right)\mathrm{\alpha }\mathrm{\xi }+{\mathrm{\Psi }}_2\left(\mathrm{x},\mathrm{y},\mathrm{z},\mathrm{t}\right)\mathrm{\beta }\mathrm{\xi }+{\mathrm{\Psi }}_3\left(\mathrm{x},\mathrm{y},\mathrm{z},\mathrm{t}\right)\mathrm{\alpha }\mathrm{\eta }+{\mathrm{\Psi }}_4\left(\mathrm{x},\mathrm{y},\mathrm{z},\mathrm{t}\right)\mathrm{\beta }\mathrm{\eta }$$

(10)

In fact, the four coupled partial differential equations in (10) can be transformed into two coupled partial differential equations, since ${\mathrm{\Psi }}_1$ and ${\mathrm{\Psi }}_2$ as ${\mathrm{\Psi }}_3$ and ${\mathrm{\Psi }}_4$ are interchangeable. The stationary solutions of the above equation are sought in the following form:

$$\mathrm{\Psi }=\mathrm{\Phi }\left(\mathrm{x},\mathrm{y},\mathrm{z},\mathrm{r},\mathrm{s}\right){\mathrm{e}}^{-{\displaystyle \frac{\mathrm{i}}{\hslash }}\mathrm{E}\mathrm{t}}$$

(11)

The corresponding derivations can be found in many quantum mechanics literature (Aitchinson [5], Bjorken [6], Bohm [7], Hameka [8], Kilmister [9]). Taking the above into account, we have to solve an eigenvalue equation, where Ψ can be written in the following form:

$$\mathrm{\Psi }={\displaystyle \frac{1}{\mathrm{r}}}\left[\begin{array}{c}\mathrm{F}(\mathrm{r})\\ \mathrm{G}(\mathrm{r})\end{array}\right]$$

(12)

The corresponding mathematical procedures lead to a system of equations consisting of two ordinary differential equations, the solution of which can be basically carried out according to the literature on quantum mechanics:

$${\displaystyle \frac{\mathrm{d}\mathrm{G}}{\mathrm{d}\mathrm{r}}}-\mathrm{K}{\displaystyle \frac{\mathrm{G}}{\mathrm{r}}}={\displaystyle \frac{1}{\hslash \mathrm{c}}}\left({\mathrm{\mu }}_0{\mathrm{c}}^2-\mathrm{E}+\mathrm{U}(\mathrm{r})\right)\mathrm{F}$$

(13)

$${\displaystyle \frac{\mathrm{d}\mathrm{F}}{\mathrm{d}\mathrm{r}}}+\mathrm{K}{\displaystyle \frac{\mathrm{F}}{\mathrm{r}}}={\displaystyle \frac{1}{\hslash \mathrm{c}}}\left({\mathrm{\mu }}_0{\mathrm{c}}^2+\mathrm{E}-\mathrm{U}(\mathrm{r})\right)\mathrm{G}$$

(14)

where

$$\mathrm{K}=\mp \left(\mathrm{j}+{\displaystyle \frac{1}{2}}\right)$$

(15)

The derivation presented so far is fully consistent with the details of the literature cited above. Details of the differences in U(r) are given in the next section. The solution of the radial equations is available in many books on quantum mechanics. The only important purpose of the detailed description of the solution presented here is to point out the point where the original quantum mechanical interpretation can be changed to a more general interpretation of “large-scale systems”. We now extend the interpretation of U(r) to include the gravitational potential in the potential energy:

$$\mathrm{U}(\mathrm{r})=-{\displaystyle \frac{1}{\mathrm{r}}}({\mathrm{e}}^2+{\mathrm{f}}_{\mathrm{x}}\mathrm{M}{\mathrm{\mu }}_0)$$

(16)

$${\displaystyle \frac{1}{\hslash \mathrm{c}}}\mathrm{U}(\mathrm{r})=-{\displaystyle \frac{1}{\mathrm{r}}}\mathrm{A}$$

(17)

where due to the correct dimensions:

$$\mathrm{A}={\displaystyle \frac{1}{4\mathrm{\pi }{\mathrm{\epsilon }}_0}}{\displaystyle \frac{{\mathrm{e}}^2}{\hslash \mathrm{c}}}\mathrm{Z}+{\mathrm{f}}_{\mathrm{x}}{\displaystyle \frac{\mathrm{M}{\mathrm{\mu }}_0}{\hslash \mathrm{c}}}$$

(18)

Here, f_x is the gravitational constant. In the following, “A” will play a role in the interpretation of (19). We assume Z=1 and substitute back into (14) and (15):

$${\displaystyle \frac{\mathrm{d}\mathrm{G}}{\mathrm{d}\mathrm{r}}}-\mathrm{K}{\displaystyle \frac{\mathrm{G}}{\mathrm{r}}}=\left({\displaystyle \frac{{\mathrm{\mu }}_0\mathrm{c}}{\hslash }}(1-{\displaystyle \frac{\mathrm{E}}{{\mathrm{\mu }}_0{\mathrm{c}}^2}})-\mathrm{A}{\displaystyle \frac{1}{\mathrm{r}}}\right)\mathrm{F}$$

(19)

$${\displaystyle \frac{\mathrm{d}\mathrm{F}}{\mathrm{d}\mathrm{r}}}+\mathrm{K}{\displaystyle \frac{\mathrm{F}}{\mathrm{r}}}=\left({\displaystyle \frac{{\mathrm{\mu }}_0\mathrm{c}}{\hslash }}(1+{\displaystyle \frac{\mathrm{E}}{{\mathrm{\mu }}_0{\mathrm{c}}^2}})+\mathrm{A}{\displaystyle \frac{1}{\mathrm{r}}}\right)\mathrm{G}$$

(20)

The solution procedure follows the descriptions in the literature, i.e, the form of the asymptotic solution (given by a large r-value) is:

$$\begin{array}{l}\mathrm{F}=\mathrm{r}\mathrm{f}\\ \mathrm{G}=\mathrm{r}\mathrm{g}\end{array}$$

(21)

where, following the literature and summerized:

$$\mathrm{\lambda }={\displaystyle \frac{{\mathrm{\mu }}_0\mathrm{c}}{\hslash }}\sqrt{1-{\mathrm{\epsilon }}^2}$$

$${\mathrm{E}}_0={\mathrm{\mu }}_0{\mathrm{c}}^2$$

$$\mathrm{\epsilon }={\displaystyle \frac{\mathrm{E}}{{\mathrm{E}}_0}}$$

$$\mathrm{x}=2\mathrm{\lambda }\mathrm{r}$$

$${\displaystyle \frac{1}{\mathrm{r}}}=2\mathrm{\lambda }{\displaystyle \frac{1}{\mathrm{x}}}$$

$$\mathrm{d}\mathrm{x}=2\mathrm{\lambda }\mathrm{d}\mathrm{r}$$

(22)

Based on the above:

$${\displaystyle \frac{\mathrm{d}\mathrm{G}}{\mathrm{d}\mathrm{r}}}={\displaystyle \frac{\mathrm{d}\mathrm{G}}{\mathrm{d}\mathrm{x}}}{\displaystyle \frac{\mathrm{d}\mathrm{x}}{\mathrm{d}\mathrm{r}}}=2\mathrm{\lambda }{\displaystyle \frac{\mathrm{d}\mathrm{G}}{\mathrm{d}\mathrm{x}}}$$

(23)

likewise:

$${\displaystyle \frac{\mathrm{d}\mathrm{F}}{\mathrm{d}\mathrm{r}}}={\displaystyle \frac{\mathrm{d}\mathrm{F}}{\mathrm{d}\mathrm{x}}}{\displaystyle \frac{\mathrm{d}\mathrm{x}}{\mathrm{d}\mathrm{r}}}=2\mathrm{\lambda }{\displaystyle \frac{\mathrm{d}\mathrm{F}}{\mathrm{d}\mathrm{x}}}$$

(24)

Substitute equations (23) and (24) into equations (19) and (20):

$$2\mathrm{\lambda }{\displaystyle \frac{\mathrm{d}\mathrm{G}}{\mathrm{d}\mathrm{x}}}-\mathrm{K}{\displaystyle \frac{\mathrm{G}}{\mathrm{x}}}2\mathrm{\lambda }=\left({\displaystyle \frac{{\mathrm{\mu }}_0\mathrm{c}}{\hslash }}(1-{\displaystyle \frac{\mathrm{E}}{{\mathrm{\mu }}_0{\mathrm{c}}^2}})-\mathrm{A}\cdot 2\mathrm{\lambda }{\displaystyle \frac{1}{\mathrm{x}}}\right)\mathrm{F}$$

(25)

$$2\mathrm{\lambda }{\displaystyle \frac{\mathrm{d}\mathrm{F}}{\mathrm{d}\mathrm{x}}}+\mathrm{K}{\displaystyle \frac{\mathrm{F}}{\mathrm{x}}}2\mathrm{\lambda }=\left({\displaystyle \frac{{\mathrm{\mu }}_0\mathrm{c}}{\hslash }}(1+{\displaystyle \frac{\mathrm{E}}{{\mathrm{\mu }}_0{\mathrm{c}}^2}})+\mathrm{A}\cdot 2\mathrm{\lambda }{\displaystyle \frac{1}{\mathrm{x}}}\right)\mathrm{G}$$

(26)

Continue with the simplifications, dividing the equations by 2λ:

$${\displaystyle \frac{\mathrm{d}\mathrm{G}}{\mathrm{d}\mathrm{x}}}-\mathrm{K}{\displaystyle \frac{\mathrm{G}}{\mathrm{x}}}=\left({\displaystyle \frac{1}{2\mathrm{\lambda }}}{\displaystyle \frac{{\mathrm{\mu }}_0\mathrm{c}}{\hslash }}(1-\mathrm{\epsilon })-\mathrm{A}{\displaystyle \frac{1}{\mathrm{x}}}\right)\mathrm{F}$$

(27)

$${\displaystyle \frac{\mathrm{d}\mathrm{F}}{\mathrm{d}\mathrm{x}}}+\mathrm{K}{\displaystyle \frac{\mathrm{F}}{\mathrm{x}}}=\left({\displaystyle \frac{1}{2\mathrm{\lambda }}}{\displaystyle \frac{{\mathrm{\mu }}_0\mathrm{c}}{\hslash }}(1+\mathrm{\epsilon })+\mathrm{A}{\displaystyle \frac{1}{\mathrm{x}}}\right)\mathrm{G}$$

(28)

Substituting (22) and with minor modifications (27), we can write:

$${\displaystyle \frac{1}{\sqrt{1-\mathrm{\epsilon }}}}\left({\displaystyle \frac{\mathrm{d}\mathrm{G}}{\mathrm{d}\mathrm{x}}}-\mathrm{K}{\displaystyle \frac{\mathrm{G}}{\mathrm{x}}}\right)=\left({\displaystyle \frac{\hslash }{2{\mathrm{\mu }}_0\mathrm{c}}}{\displaystyle \frac{{\mathrm{\mu }}_0\mathrm{c}}{\hslash }}{\displaystyle \frac{\sqrt{1-\mathrm{\epsilon }}\sqrt{1-\mathrm{\epsilon }}}{\sqrt{1-\mathrm{\epsilon }}\sqrt{1+\mathrm{\epsilon }}}}{\displaystyle \frac{\sqrt{1+\mathrm{\epsilon }}}{\sqrt{1-\mathrm{\epsilon }}}}-\mathrm{A}{\displaystyle \frac{\sqrt{1+\mathrm{\epsilon }}}{\sqrt{1-\mathrm{\epsilon }}}}{\displaystyle \frac{1}{\mathrm{x}}}\right)\mathrm{F}{\displaystyle \frac{1}{\sqrt{1+\mathrm{\epsilon }}}}$$

(29)

After simplifications:

$${\displaystyle \frac{1}{\sqrt{1-\mathrm{\epsilon }}}}\left({\displaystyle \frac{\mathrm{d}\mathrm{G}}{\mathrm{d}\mathrm{x}}}-\mathrm{K}{\displaystyle \frac{\mathrm{G}}{\mathrm{x}}}\right)=\left({\displaystyle \frac{1}{2}}-\mathrm{A}{\displaystyle \frac{\sqrt{1+\mathrm{\epsilon }}}{\sqrt{1-\mathrm{\epsilon }}}}{\displaystyle \frac{1}{\mathrm{x}}}\right)\mathrm{F}{\displaystyle \frac{1}{\sqrt{1+\mathrm{\epsilon }}}}$$

(30)

Similarly, substituting (22) with minor modifications, (28) can be written:

$${\displaystyle \frac{1}{\sqrt{1+\mathrm{\epsilon }}}}\left({\displaystyle \frac{\mathrm{d}\mathrm{F}}{\mathrm{d}\mathrm{x}}}+\mathrm{K}{\displaystyle \frac{\mathrm{F}}{\mathrm{x}}}\right)=\left({\displaystyle \frac{\hslash }{2{\mathrm{\mu }}_0\mathrm{c}}}{\displaystyle \frac{{\mathrm{\mu }}_0\mathrm{c}}{\hslash }}{\displaystyle \frac{\sqrt{1+\mathrm{\epsilon }}\sqrt{1+\mathrm{\epsilon }}}{\sqrt{1-\mathrm{\epsilon }}\sqrt{1+\mathrm{\epsilon }}}}{\displaystyle \frac{\sqrt{1-\mathrm{\epsilon }}}{\sqrt{1+\mathrm{\epsilon }}}}+\mathrm{A}{\displaystyle \frac{\sqrt{1-\mathrm{\epsilon }}}{\sqrt{1+\mathrm{\epsilon }}}}{\displaystyle \frac{1}{\mathrm{x}}}\right)\mathrm{G}{\displaystyle \frac{1}{\sqrt{1-\mathrm{\epsilon }}}}$$

(31)

After simplifications:

$${\displaystyle \frac{1}{\sqrt{1+\mathrm{\epsilon }}}}\left({\displaystyle \frac{\mathrm{d}\mathrm{F}}{\mathrm{d}\mathrm{x}}}+\mathrm{K}{\displaystyle \frac{\mathrm{F}}{\mathrm{x}}}\right)=\left({\displaystyle \frac{1}{2}}+\mathrm{A}{\displaystyle \frac{\sqrt{1-\mathrm{\epsilon }}}{\sqrt{1+\mathrm{\epsilon }}}}{\displaystyle \frac{1}{\mathrm{x}}}\right)\mathrm{G}{\displaystyle \frac{1}{\sqrt{1-\mathrm{\epsilon }}}}$$

(32)

We have to solve the coupled equations (30) and (32). According to mathematicians the solution should be found in the following form:

$$\mathrm{G}=\sqrt{1-\mathrm{\epsilon }}\cdot {\mathrm{e}}^{-{\displaystyle \frac{1}{2}}\mathrm{x}}\left({\mathrm{\phi }}_1-{\mathrm{\phi }}_2\right)$$

(33)

$$\mathrm{F}=\sqrt{1+\mathrm{\epsilon }}\cdot {\mathrm{e}}^{-{\displaystyle \frac{1}{2}}\mathrm{x}}\left({\mathrm{\phi }}_1+{\mathrm{\phi }}_2\right)$$

(34)

Form the derivatives of (33) and (34):

$${\displaystyle \frac{\mathrm{d}\mathrm{G}}{\mathrm{d}\mathrm{x}}}=\sqrt{1-\mathrm{\epsilon }}\cdot {\mathrm{e}}^{-{\displaystyle \frac{1}{2}}\mathrm{x}}\left(-{\displaystyle \frac{1}{2}}{\mathrm{\phi }}_1+{\displaystyle \frac{1}{2}}{\mathrm{\phi }}_2+{\displaystyle \frac{\mathrm{d}{\mathrm{\phi }}_1}{\mathrm{d}\mathrm{x}}}-{\displaystyle \frac{\mathrm{d}{\mathrm{\phi }}_2}{\mathrm{d}\mathrm{x}}}\right)$$

(35)

$${\displaystyle \frac{\mathrm{d}\mathrm{F}}{\mathrm{d}\mathrm{x}}}=\sqrt{1+\mathrm{\epsilon }}\cdot {\mathrm{e}}^{-{\displaystyle \frac{1}{2}}\mathrm{x}}\left(-{\displaystyle \frac{1}{2}}{\mathrm{\phi }}_1-{\displaystyle \frac{1}{2}}{\mathrm{\phi }}_2+{\displaystyle \frac{\mathrm{d}{\mathrm{\phi }}_1}{\mathrm{d}\mathrm{x}}}+{\displaystyle \frac{\mathrm{d}{\mathrm{\phi }}_2}{\mathrm{d}\mathrm{x}}}\right)$$

(36)

Substitute (33), (34), and (35) into (32):

$$\begin{array}{l}{\displaystyle \frac{1}{\sqrt{1-\mathrm{\epsilon }}}}\left(\sqrt{1-\mathrm{\epsilon }}\cdot {\mathrm{e}}^{-{\displaystyle \frac{1}{2}}\mathrm{x}}\left(-{\displaystyle \frac{1}{2}}{\mathrm{\phi }}_1+{\displaystyle \frac{1}{2}}{\mathrm{\phi }}_2+{\displaystyle \frac{\mathrm{d}{\mathrm{\phi }}_1}{\mathrm{d}\mathrm{x}}}-{\displaystyle \frac{\mathrm{d}{\mathrm{\phi }}_2}{\mathrm{d}\mathrm{x}}}\right)-{\displaystyle \frac{\mathrm{K}}{\mathrm{x}}}\sqrt{1-\mathrm{\epsilon }}\cdot {\mathrm{e}}^{-{\displaystyle \frac{1}{2}}\mathrm{x}}\left({\mathrm{\phi }}_1-{\mathrm{\phi }}_2\right)\right)\\ =\left({\displaystyle \frac{1}{2}}-\mathrm{A}{\displaystyle \frac{\sqrt{1+\mathrm{\epsilon }}}{\sqrt{1-\mathrm{\epsilon }}}}{\displaystyle \frac{1}{\mathrm{x}}}\right){\displaystyle \frac{1}{\sqrt{1+\mathrm{\epsilon }}}}\sqrt{1+\mathrm{\epsilon }}\cdot {\mathrm{e}}^{-{\displaystyle \frac{1}{2}}\mathrm{x}}\left({\mathrm{\phi }}_1+{\mathrm{\phi }}_2\right)\end{array}$$

(37)

We can simplify with ${\mathrm{e}}^{-{\displaystyle \frac{1}{2}}\mathrm{x}}$:

$$-{\displaystyle \frac{1}{2}}{\mathrm{\phi }}_1+{\displaystyle \frac{1}{2}}{\mathrm{\phi }}_2+{\displaystyle \frac{\mathrm{d}{\mathrm{\phi }}_1}{\mathrm{d}\mathrm{x}}}-{\displaystyle \frac{\mathrm{d}{\mathrm{\phi }}_2}{\mathrm{d}\mathrm{x}}}-{\displaystyle \frac{\mathrm{K}}{\mathrm{x}}}\left({\mathrm{\phi }}_1-{\mathrm{\phi }}_2\right)=\left({\displaystyle \frac{1}{2}}-\mathrm{A}{\displaystyle \frac{\sqrt{1+\mathrm{\epsilon }}}{\sqrt{1-\mathrm{\epsilon }}}}{\displaystyle \frac{1}{\mathrm{x}}}\right)\left({\mathrm{\phi }}_1+{\mathrm{\phi }}_2\right)$$

(38)

$$-{\displaystyle \frac{1}{2}}{\mathrm{\phi }}_1+{\displaystyle \frac{1}{2}}{\mathrm{\phi }}_2+{\displaystyle \frac{\mathrm{d}{\mathrm{\phi }}_1}{\mathrm{d}\mathrm{x}}}-{\displaystyle \frac{\mathrm{d}{\mathrm{\phi }}_2}{\mathrm{d}\mathrm{x}}}-{\displaystyle \frac{\mathrm{K}}{\mathrm{x}}}\left({\mathrm{\phi }}_1-{\mathrm{\phi }}_2\right)={\displaystyle \frac{1}{2}}{\mathrm{\phi }}_1-\mathrm{A}{\displaystyle \frac{\sqrt{1+\mathrm{\epsilon }}}{\sqrt{1-\mathrm{\epsilon }}}}{\displaystyle \frac{1}{\mathrm{x}}}{\mathrm{\phi }}_1+{\displaystyle \frac{1}{2}}{\mathrm{\phi }}_2-\mathrm{A}{\displaystyle \frac{\sqrt{1+\mathrm{\epsilon }}}{\sqrt{1-\mathrm{\epsilon }}}}{\displaystyle \frac{1}{\mathrm{x}}}{\mathrm{\phi }}_2$$

(39)

Simplifying it further:

$${\displaystyle \frac{\mathrm{d}{\mathrm{\phi }}_1}{\mathrm{d}\mathrm{x}}}-{\displaystyle \frac{\mathrm{d}{\mathrm{\phi }}_2}{\mathrm{d}\mathrm{x}}}={\mathrm{\phi }}_1\left(1+{\displaystyle \frac{\mathrm{K}}{\mathrm{x}}}-\mathrm{A}{\displaystyle \frac{\sqrt{1+\mathrm{\epsilon }}}{\sqrt{1-\mathrm{\epsilon }}}}{\displaystyle \frac{1}{\mathrm{x}}}\right)+{\mathrm{\phi }}_2\left(-{\displaystyle \frac{\mathrm{K}}{\mathrm{x}}}-\mathrm{A}{\displaystyle \frac{\sqrt{1+\mathrm{\epsilon }}}{\sqrt{1-\mathrm{\epsilon }}}}{\displaystyle \frac{1}{\mathrm{x}}}\right)$$

(40)

Now we do the same with (33), (34), and (36), substituting into (32):

$$\begin{array}{l}{\displaystyle \frac{1}{\sqrt{1+\mathrm{\epsilon }}}}\left(\sqrt{1+\mathrm{\epsilon }}\cdot {\mathrm{e}}^{-{\displaystyle \frac{1}{2}}\mathrm{x}}\left(-{\displaystyle \frac{1}{2}}{\mathrm{\phi }}_1-{\displaystyle \frac{1}{2}}{\mathrm{\phi }}_2+{\displaystyle \frac{\mathrm{d}{\mathrm{\phi }}_1}{\mathrm{d}\mathrm{x}}}+{\displaystyle \frac{\mathrm{d}{\mathrm{\phi }}_2}{\mathrm{d}\mathrm{x}}}\right)+{\displaystyle \frac{\mathrm{K}}{\mathrm{x}}}\sqrt{1+\mathrm{\epsilon }}\cdot {\mathrm{e}}^{-{\displaystyle \frac{1}{2}}\mathrm{x}}\left({\mathrm{\phi }}_1+{\mathrm{\phi }}_2\right)\right)\\ =\left({\displaystyle \frac{1}{2}}+\mathrm{A}{\displaystyle \frac{\sqrt{1-\mathrm{\epsilon }}}{\sqrt{1+\mathrm{\epsilon }}}}{\displaystyle \frac{1}{\mathrm{x}}}\right){\displaystyle \frac{1}{\sqrt{1-\mathrm{\epsilon }}}}\sqrt{1-\mathrm{\epsilon }}\cdot {\mathrm{e}}^{-{\displaystyle \frac{1}{2}}\mathrm{x}}\left({\mathrm{\phi }}_1-{\mathrm{\phi }}_2\right)\end{array}$$

(41)

Simplified again with ${\mathrm{e}}^{-{\displaystyle \frac{1}{2}}\mathrm{x}}$:

$$-{\displaystyle \frac{1}{2}}{\mathrm{\phi }}_1-{\displaystyle \frac{1}{2}}{\mathrm{\phi }}_2+{\displaystyle \frac{\mathrm{d}{\mathrm{\phi }}_1}{\mathrm{d}\mathrm{x}}}+{\displaystyle \frac{\mathrm{d}{\mathrm{\phi }}_2}{\mathrm{d}\mathrm{x}}}+{\displaystyle \frac{\mathrm{K}}{\mathrm{x}}}\left({\mathrm{\phi }}_1+{\mathrm{\phi }}_2\right)=\left({\displaystyle \frac{1}{2}}+\mathrm{A}{\displaystyle \frac{\sqrt{1-\mathrm{\epsilon }}}{\sqrt{1+\mathrm{\epsilon }}}}{\displaystyle \frac{1}{\mathrm{x}}}\right)\left({\mathrm{\phi }}_1-{\mathrm{\phi }}_2\right)$$

(42)

$$\begin{array}{l}-{\displaystyle \frac{1}{2}}{\mathrm{\phi }}_1-{\displaystyle \frac{1}{2}}{\mathrm{\phi }}_2+{\displaystyle \frac{\mathrm{d}{\mathrm{\phi }}_1}{\mathrm{d}\mathrm{x}}}+{\displaystyle \frac{\mathrm{d}{\mathrm{\phi }}_2}{\mathrm{d}\mathrm{x}}}+{\displaystyle \frac{\mathrm{K}}{\mathrm{x}}}\left({\mathrm{\phi }}_1+{\mathrm{\phi }}_2\right)=\\ ={\displaystyle \frac{1}{2}}{\mathrm{\phi }}_1+\mathrm{A}{\displaystyle \frac{\sqrt{1-\mathrm{\epsilon }}}{\sqrt{1+\mathrm{\epsilon }}}}{\displaystyle \frac{1}{\mathrm{x}}}{\mathrm{\phi }}_1-{\displaystyle \frac{1}{2}}{\mathrm{\phi }}_2-\mathrm{A}{\displaystyle \frac{\sqrt{1-\mathrm{\epsilon }}}{\sqrt{1+\mathrm{\epsilon }}}}{\displaystyle \frac{1}{\mathrm{x}}}{\mathrm{\phi }}_2\end{array}$$

(43)

Simplifying it further:

$${\displaystyle \frac{\mathrm{d}{\mathrm{\phi }}_1}{\mathrm{d}\mathrm{x}}}+{\displaystyle \frac{\mathrm{d}{\mathrm{\phi }}_2}{\mathrm{d}\mathrm{x}}}={\mathrm{\phi }}_1\left(1-{\displaystyle \frac{\mathrm{K}}{\mathrm{x}}}+\mathrm{A}{\displaystyle \frac{\sqrt{1-\mathrm{\epsilon }}}{\sqrt{1+\mathrm{\epsilon }}}}{\displaystyle \frac{1}{\mathrm{x}}}\right)+{\mathrm{\phi }}_2\left(-{\displaystyle \frac{\mathrm{K}}{\mathrm{x}}}-\mathrm{A}{\displaystyle \frac{\sqrt{1-\mathrm{\epsilon }}}{\sqrt{1+\mathrm{\epsilon }}}}{\displaystyle \frac{1}{\mathrm{x}}}\right)$$

(44)

Let equations (40) and (44) be added:

$$2{\displaystyle \frac{\mathrm{d}{\mathrm{\phi }}_1}{\mathrm{d}\mathrm{x}}}={\mathrm{\phi }}_1\left(2-{\displaystyle \frac{\mathrm{K}}{\mathrm{x}}}+{\displaystyle \frac{\mathrm{K}}{\mathrm{x}}}+\left({\displaystyle \frac{\sqrt{1-\mathrm{\epsilon }}}{\sqrt{1+\mathrm{\epsilon }}}}-{\displaystyle \frac{\sqrt{1+\mathrm{\epsilon }}}{\sqrt{1-\mathrm{\epsilon }}}}\right)\mathrm{A}{\displaystyle \frac{1}{\mathrm{x}}}\right)+{\mathrm{\phi }}_2\left(-2{\displaystyle \frac{\mathrm{K}}{\mathrm{x}}}+\left(-{\displaystyle \frac{\sqrt{1-\mathrm{\epsilon }}}{\sqrt{1+\mathrm{\epsilon }}}}-{\displaystyle \frac{\sqrt{1+\mathrm{\epsilon }}}{\sqrt{1-\mathrm{\epsilon }}}}\right)\mathrm{A}{\displaystyle \frac{1}{\mathrm{x}}}\right)$$

(45)

Simplified:

$${\displaystyle \frac{\mathrm{d}{\mathrm{\phi }}_1}{\mathrm{d}\mathrm{x}}}={\mathrm{\phi }}_1\left(1-{\displaystyle \frac{\mathrm{\epsilon }}{\sqrt{1-{\mathrm{\epsilon }}^2}}}\mathrm{A}{\displaystyle \frac{1}{\mathrm{x}}}\right)+{\mathrm{\phi }}_2\left(-{\displaystyle \frac{\mathrm{K}}{\mathrm{x}}}-{\displaystyle \frac{1}{\sqrt{1-{\mathrm{\epsilon }}^2}}}\mathrm{A}{\displaystyle \frac{1}{\mathrm{x}}}\right)$$

(46)

Subtract equation (40) from (44):

$$2{\displaystyle \frac{\mathrm{d}{\mathrm{\phi }}_2}{\mathrm{d}\mathrm{x}}}={\mathrm{\phi }}_1\left(-2{\displaystyle \frac{\mathrm{K}}{\mathrm{x}}}+\left({\displaystyle \frac{\sqrt{1-\mathrm{\epsilon }}}{\sqrt{1+\mathrm{\epsilon }}}}+{\displaystyle \frac{\sqrt{1+\mathrm{\epsilon }}}{\sqrt{1-\mathrm{\epsilon }}}}\right)\mathrm{A}{\displaystyle \frac{1}{\mathrm{x}}}\right)+{\mathrm{\phi }}_2\left(\left(-{\displaystyle \frac{\sqrt{1-\mathrm{\epsilon }}}{\sqrt{1+\mathrm{\epsilon }}}}+{\displaystyle \frac{\sqrt{1+\mathrm{\epsilon }}}{\sqrt{1-\mathrm{\epsilon }}}}\right)\mathrm{A}{\displaystyle \frac{1}{\mathrm{x}}}\right)$$

(47)

$${\displaystyle \frac{\mathrm{d}{\mathrm{\phi }}_2}{\mathrm{d}\mathrm{x}}}={\mathrm{\phi }}_1\left(-{\displaystyle \frac{\mathrm{K}}{\mathrm{x}}}+{\displaystyle \frac{\mathrm{\epsilon }}{\sqrt{1-{\mathrm{\epsilon }}^2}}}\mathrm{A}{\displaystyle \frac{1}{\mathrm{x}}}\right)+{\mathrm{\phi }}_2\left({\displaystyle \frac{\mathrm{\epsilon }}{\sqrt{1-{\mathrm{\epsilon }}^2}}}\mathrm{A}{\displaystyle \frac{1}{\mathrm{x}}}\right)$$

(48)

Let us continue with equations (46) and (48). Find the functions in power series form:

$${\mathrm{\phi }}_1={\mathrm{x}}^{\mathrm{s}}{\displaystyle \sum _{\mathrm{p}=0}^{\infty }{\mathrm{a}{}_{\mathrm{p}}\mathrm{x}}^{\mathrm{p}}}$$

$$\mathrm{and}{\mathrm{\phi }}_2={\mathrm{x}}^{\mathrm{s}}{\displaystyle \sum _{\mathrm{p}=0}^{\infty }\mathrm{b}{{}_{\mathrm{p}}\mathrm{x}}^{\mathrm{p}}}$$

(49)

Express φ₁ in (49) and form the derivative:

$${\mathrm{\phi }}_1={\mathrm{a}}_0{\mathrm{x}}^{\mathrm{s}}+{\mathrm{a}}_1{\mathrm{x}}^{\mathrm{s}+1}+{\mathrm{a}}_2{\mathrm{x}}^{\mathrm{s}+2}\mathrm{.....}$$

(50)

$${\displaystyle \frac{\mathrm{d}{\mathrm{\phi }}_1}{\mathrm{d}\mathrm{x}}}=\mathrm{s}{\mathrm{a}}_0{\mathrm{x}}^{\mathrm{s}-1}+\left(\mathrm{s}+1\right){\mathrm{a}}_1{\mathrm{x}}^{\mathrm{s}}+\left(\mathrm{s}+2\right){\mathrm{a}}_2{\mathrm{x}}^{\mathrm{s}+1}\mathrm{.....}$$

(51)

$${\displaystyle \frac{\mathrm{d}{\mathrm{\phi }}_1}{\mathrm{d}\mathrm{x}}}={\displaystyle \sum _{\mathrm{p}=0}^{\infty }\left(\mathrm{s}+\mathrm{p}\right){\mathrm{a}}_{\mathrm{p}}{\mathrm{x}}^{\mathrm{s}+\mathrm{p}-1}}$$

(52)

Substitute into (46):

$${\displaystyle {\displaystyle \sum _{\mathrm{p}=0}^{\infty }}\left(\mathrm{s}+\mathrm{p}\right){\mathrm{a}}_{\mathrm{p}}{\mathrm{x}}^{\mathrm{s}+\mathrm{p}-1}}=\left(1-{\displaystyle \frac{\mathrm{\epsilon }}{\sqrt{1-{\mathrm{\epsilon }}^2}}}\mathrm{A}{\displaystyle \frac{1}{\mathrm{x}}}\right){\displaystyle {\displaystyle \sum _{\mathrm{p}=0}^{\infty }}{\mathrm{a}}_{\mathrm{p}}{\mathrm{x}}^{\mathrm{p}+\mathrm{s}}}+\left(-\mathrm{K}-{\displaystyle \frac{1}{\sqrt{1-{\mathrm{\epsilon }}^2}}}\mathrm{A}\right){\displaystyle {\displaystyle \sum _{\mathrm{p}=0}^{\infty }}{\mathrm{b}}_{\mathrm{p}}}{\mathrm{x}}^{\mathrm{p}+\mathrm{s}-1}$$

(53)

$${\displaystyle {\displaystyle \sum _{\mathrm{p}=0}^{\infty }}\left(\mathrm{s}+\mathrm{p}\right){\mathrm{a}}_{\mathrm{p}}{\mathrm{x}}^{\mathrm{s}+\mathrm{p}-1}}={\displaystyle {\displaystyle \sum _{\mathrm{p}=0}^{\infty }}{\mathrm{a}}_{\mathrm{p}}{\mathrm{x}}^{\mathrm{p}+\mathrm{s}}}-{\displaystyle \frac{\mathrm{\epsilon }}{\sqrt{1-{\mathrm{\epsilon }}^2}}}\mathrm{A}{\displaystyle {\displaystyle \sum _{\mathrm{p}=0}^{\infty }}{\mathrm{a}}_{\mathrm{p}}{\mathrm{x}}^{\mathrm{p}+\mathrm{s}-1}}-\left(\mathrm{K}+{\displaystyle \frac{1}{\sqrt{1-{\mathrm{\epsilon }}^2}}}\mathrm{A}\right){\displaystyle {\displaystyle \sum _{\mathrm{p}=0}^{\infty }}{\mathrm{b}}_{\mathrm{p}}}{\mathrm{x}}^{\mathrm{p}+\mathrm{s}-1}$$

(54)

Now we can write the following for the coefficients ${\mathrm{x}}^{\mathrm{s}+\mathrm{p}-1}$:

$$\left(\mathrm{s}+\mathrm{p}\right){\mathrm{a}}_{\mathrm{p}}={\mathrm{a}}_{\mathrm{p}-1}-{\displaystyle \frac{\mathrm{\epsilon }}{\sqrt{1-{\mathrm{\epsilon }}^2}}}\mathrm{A}{\mathrm{a}}_{\mathrm{p}}-\left(\mathrm{K}+{\displaystyle \frac{1}{\sqrt{1-{\mathrm{\epsilon }}^2}}}\mathrm{A}\right){\mathrm{b}}_{\mathrm{p}}$$

(55)

Expressing φ₂ in (49) similarly to (50), we obtain:

$${\mathrm{\phi }}_2={\mathrm{b}}_0{\mathrm{x}}^{\mathrm{s}}+{\mathrm{b}}_1{\mathrm{x}}^{\mathrm{s}+1}+{\mathrm{b}}_2{\mathrm{x}}^{\mathrm{s}+2}\mathrm{.....}$$

(56)

$${\displaystyle \frac{\mathrm{d}{\mathrm{\phi }}_2}{\mathrm{d}\mathrm{x}}}=\mathrm{s}{\mathrm{b}}_0{\mathrm{x}}^{\mathrm{s}-1}+\left(\mathrm{s}+1\right){\mathrm{b}}_1{\mathrm{x}}^{\mathrm{s}}+\left(\mathrm{s}+2\right){\mathrm{b}}_2{\mathrm{x}}^{\mathrm{s}+1}\mathrm{.....}$$

(57)

$${\displaystyle \frac{\mathrm{d}{\mathrm{\phi }}_2}{\mathrm{d}\mathrm{x}}}={\displaystyle \sum _{\mathrm{p}=0}^{\infty }\left(\mathrm{s}+\mathrm{p}\right){\mathrm{b}}_{\mathrm{p}}{\mathrm{x}}^{\mathrm{s}+\mathrm{p}-1}}$$

(58)

Substituted in (48):

$${\displaystyle {\displaystyle \sum _{\mathrm{p}=0}^{\infty }}\left(\mathrm{s}+\mathrm{p}\right){\mathrm{b}}_{\mathrm{p}}{\mathrm{x}}^{\mathrm{s}+\mathrm{p}-1}}=\left(-\mathrm{K}+{\displaystyle \frac{1}{\sqrt{1-{\mathrm{\epsilon }}^2}}}\mathrm{A}\right){\displaystyle {\displaystyle \sum _{\mathrm{p}=0}^{\infty }}{\mathrm{a}}_{\mathrm{p}}{\mathrm{x}}^{\mathrm{p}+\mathrm{s}-1}}+\left({\displaystyle \frac{\mathrm{\epsilon }}{\sqrt{1-{\mathrm{\epsilon }}^2}}}\mathrm{A}\right){\displaystyle {\displaystyle \sum _{\mathrm{p}=0}^{\infty }}{\mathrm{b}}_{\mathrm{p}}}{\mathrm{x}}^{\mathrm{p}+\mathrm{s}-1}$$

(59)

Now we can write the following for the coefficients ${\mathrm{x}}^{\mathrm{s}+\mathrm{p}-1}$:

$$\left(\mathrm{s}+\mathrm{p}\right){\mathrm{b}}_{\mathrm{p}}=\left(-\mathrm{K}+{\displaystyle \frac{1}{\sqrt{1-{\mathrm{\epsilon }}^2}}}\mathrm{A}\right){\mathrm{a}}_{\mathrm{p}}+{\displaystyle \frac{\mathrm{\epsilon }}{\sqrt{1-{\mathrm{\epsilon }}^2}}}\mathrm{A}{\mathrm{b}}_{\mathrm{p}}$$

(60)

Equations (55) and (60), for p=0:

$${\mathrm{a}}_0\mathrm{s}={\mathrm{a}}_{-1}-{\displaystyle \frac{\mathrm{\epsilon }}{\sqrt{1-{\mathrm{\epsilon }}^2}}}\mathrm{A}{\mathrm{a}}_0-\left(\mathrm{K}+{\displaystyle \frac{1}{\sqrt{1-{\mathrm{\epsilon }}^2}}}\mathrm{A}\right){\mathrm{b}}_0$$

(61)

$${\mathrm{b}}_0\mathrm{s}=\left(-\mathrm{K}+{\displaystyle \frac{1}{\sqrt{1-{\mathrm{\epsilon }}^2}}}\mathrm{A}\right){\mathrm{a}}_0+{\displaystyle \frac{\mathrm{\epsilon }}{\sqrt{1-{\mathrm{\epsilon }}^2}}}\mathrm{A}{\mathrm{b}}_0$$

(62)

After ${\mathrm{a}}_{-1}=0$:

$${\mathrm{a}}_0\left(\mathrm{s}+{\displaystyle \frac{\mathrm{\epsilon }}{\sqrt{1-{\mathrm{\epsilon }}^2}}}\mathrm{A}\right)+{\mathrm{b}}_0\left(\mathrm{K}+{\displaystyle \frac{1}{\sqrt{1-{\mathrm{\epsilon }}^2}}}\mathrm{A}\right)=0$$

(63)

$${\mathrm{a}}_0\left(\mathrm{K}-{\displaystyle \frac{1}{\sqrt{1-{\mathrm{\epsilon }}^2}}}\mathrm{A}\right)+{\mathrm{b}}_0\left(\mathrm{s}-{\displaystyle \frac{\mathrm{\epsilon }}{\sqrt{1-{\mathrm{\epsilon }}^2}}}\mathrm{A}\right)=0$$

(64)

The system of equations (63) and (64) has a solution if the determinant of the coefficients is zero, i.e.:

$$\left|\begin{array}{cc}\mathrm{s}+{\displaystyle \frac{\mathrm{\epsilon }}{\sqrt{1-{\mathrm{\epsilon }}^2}}}\mathrm{A}& \mathrm{K}+{\displaystyle \frac{1}{\sqrt{1-{\mathrm{\epsilon }}^2}}}\mathrm{A}\\ \mathrm{K}-{\displaystyle \frac{1}{\sqrt{1-{\mathrm{\epsilon }}^2}}}\mathrm{A}& \mathrm{s}-{\displaystyle \frac{\mathrm{\epsilon }}{\sqrt{1-{\mathrm{\epsilon }}^2}}}\mathrm{A}\end{array}\right|=0$$

(65)

The determinant value is expressed as:

$${\mathrm{s}}^2-{\displaystyle \frac{{\mathrm{\epsilon }}^2}{1-{\mathrm{\epsilon }}^2}}{\mathrm{A}}^2-\left({\mathrm{K}}^2-{\displaystyle \frac{1}{1-{\mathrm{\epsilon }}^2}}{\mathrm{A}}^2\right)=0$$

(66)

$${\mathrm{s}}^2-{\mathrm{K}}^2-\left({\displaystyle \frac{{\mathrm{\epsilon }}^2}{1-{\mathrm{\epsilon }}^2}}-{\displaystyle \frac{1}{1-{\mathrm{\epsilon }}^2}}\right){\mathrm{A}}^2=0$$

(67)

$${\mathrm{s}}^2-{\mathrm{K}}^2+{\mathrm{A}}^2=0$$

(68)

$$\mathrm{s}=\pm \sqrt{{\mathrm{K}}^2-{\mathrm{A}}^2}$$

(69)

Only a positive sign is possible, i.e.:

$$\mathrm{s}=\sqrt{{\mathrm{K}}^2-{\mathrm{A}}^2}$$

(70)

It is, in fact, partly because of this short relation (70) that the above derivation is presented in such detail. It is from this result that we can now derive the new ‘solar system constant’ or a new ‘constant of the Universe’, H_x.

4. Approximation of H_x Values

4.1. The Value of H_x from Relativistic Quantum Mechanics

So far, at least according to the mathematical formulae, there is no deviation from the usual quantum mechanical derivations. Let us take a closer look at equation (70) above. From the previous (15) and (18), it can be seen that

$\mathrm{A}={\displaystyle \frac{1}{4\mathrm{\pi }{\mathrm{\epsilon }}_0}}{\displaystyle \frac{{\mathrm{e}}^2}{\hslash \mathrm{c}}}\mathrm{Z}+{\mathrm{f}}_{\mathrm{x}}{\displaystyle \frac{\mathrm{M}{\mathrm{\mu }}_0}{\hslash \mathrm{c}}}$see previous (15)

$\mathrm{K}=\mp \left(\mathrm{j}+{\displaystyle \frac{1}{2}}\right)$see previous (18)

Furthermore, the correlation under the root (70) must be positive. At the scale of the atomic dimensions, after the substitutions, the value of A is 1/137.037 (the usual notation in quantum mechanics is α, a dimensionless number). Since j=0 is the mathematically smallest possible value in (15), this gives K=1/2, and A≤1/2 follows.

If solar system-like systems (stars and planets) could be considered systems that can be described by quantum mechanics, then the following data would need to be substituted into the above equations. (We will address the legitimate doubt as to whether these systems can be described using the mathematical and physical tools of quantum mechanics in detail in Chapters 5 and 6.)

Let us examine the substitutions in solar system-like systems. We have data for one such system, these are the following known values: f_x=6,672*10^-11 [m³/kg/s²] is the gravitational constant, M=M_Sun=1,9891*10³⁰ [kg] is the mass of the Sun, c=2,997925*10⁸ [m/s] is the speed of light. The value of µ₀ may be questionable - the smaller mass, since we have a one-mass model (Z=1), can be interpreted as the total mass of all possible masses orbiting the Sun, simplified: the total mass of the planets. This value is: µ₀≅2,668992*10²⁷ [kg]. We assume that whatever the value of the charge (e), in our case, its multiplication is negligible.

Thus, ℏ is replaced by H_x for the solar system:

$${\mathrm{H}}_{\mathrm{x}}={\mathrm{f}}_{\mathrm{x}}{\displaystyle \frac{\mathrm{M}{\mathrm{\mu }}_0}{\mathrm{A}\mathrm{c}}}$$

(71)

Substituting the above, the possible minimum value of the constant for the solar system is:

H_xmin1 ≥ 0,2363*10⁴⁰ [Js]    (72)

4.2. The Value of H_x from the Schrödinger Equation

The value of the Hx coefficient can be approximated using another quantum mechanical model. Using the mathematical model of Schrödinger’s equation of quantum mechanics, the radial part of the wave function, here denoted H_x instead of ℏ, is:

$${\displaystyle \frac{{\mathrm{d}}^2\mathrm{R}}{\mathrm{d}{\mathrm{r}}^2}}+\left[{\displaystyle \frac{2\mathrm{\mu }}{{\mathrm{H}}_{\mathrm{x}}}}\left(\mathrm{E}-\mathrm{V}(\mathrm{r})-{\displaystyle \frac{\mathrm{l}\left(\mathrm{l}+1\right)}{{\mathrm{r}}^2}}\right)\right]\mathrm{R}=0$$

(73)

The total solution is the product of the radial part and the spherical part:

$$\mathrm{\phi }\left(\mathrm{r},\mathrm{\theta },\mathrm{\chi }\right)={\displaystyle \frac{1}{\mathrm{r}}}\mathrm{R}\left(\mathrm{r}\right){\mathrm{Y}}_{\mathrm{l}}^{\mathrm{m}}\left(\mathrm{\theta },\mathrm{\chi }\right)$$

(74)

The steps of the solution are derived from the referenced literature:

$$\mathrm{\phi }\left(\mathrm{r},\mathrm{\theta },\mathrm{\chi }\right)=\mathrm{C}{\displaystyle \frac{1}{\mathrm{r}}}{\mathrm{\xi }}^{\mathrm{l}+1}{\mathrm{L}}_{\mathrm{n}+1}^{\left(2\mathrm{l}+1\right)}{\mathrm{e}}^{-{\displaystyle \frac{1}{2}}\mathrm{\xi }}{\mathrm{Y}}_{\mathrm{l}}^{\mathrm{m}}\left(\mathrm{\theta },\mathrm{\chi }\right)$$

(75)

where ${\mathrm{L}}_{\mathrm{n}+1}^{\left(2\mathrm{l}+1\right)}$ the generalized Laguerre polynomials, and $\mathrm{\xi }={\displaystyle \frac{2\mathrm{r}}{\mathrm{n}{\mathrm{r}}_0}}$After appropriate derivations and normalization, the radial density function:

$$\mathrm{\rho }={\mathrm{R}}_{\mathrm{n},\mathrm{l}}^2={\mathrm{N}}_{\mathrm{n},\mathrm{l}}^2\left[{\mathrm{\xi }}^{2\mathrm{l}}{\mathrm{L}}_{\mathrm{n}+1}^{(2\mathrm{l}+1)2}\left(\mathrm{\xi }\right){\mathrm{e}}^{-{\displaystyle \frac{2\mathrm{\xi }}{2}}}\right]$$

(76)

Within this, based on the value of ξ:

$${\mathrm{r}}_0=\mathrm{n}{\displaystyle \frac{{\mathrm{H}}_{\mathrm{x}}^2}{\mathrm{\mu }}}{\displaystyle \frac{1}{\frac{{\mathrm{e}}^2}{4\mathrm{\pi }{\mathrm{\epsilon }}_0}+{\mathrm{f}}_{\mathrm{x}}\mathrm{M}\mathrm{\mu }}}$$

(77)

Neglecting the e² member and for n=1 (i.e, considering a single point of mass and no significant electric potential):

$${\mathrm{r}}_0={\displaystyle \frac{{\mathrm{H}}_{\mathrm{x}}^2}{\mathrm{\mu }}}{\displaystyle \frac{1}{{\mathrm{f}}_{\mathrm{x}}\mathrm{M}\mathrm{\mu }}}$$

(78)

Let’s express H_x:

$${\mathrm{H}}_{\mathrm{x}}\ge \mathrm{\mu }\sqrt{{\mathrm{r}}_0\mathrm{M}{\mathrm{f}}_{\mathrm{x}}}$$

(79)

In our model, M is the central mass (the mass of the Sun), µ is the mass of a particle (the mass of a planet), and r₀ is the distance of the particle µ from the central mass M. In our case, f_x= 6,672*10^-11 [m³/kg/s²] is the gravitational constant, M = 1,9891*10³⁰ [kg] is the mass of the Sun. Here we are also dealing with a single-mass model; we can use the Earth’s mass and orbital radius data, if for no other reason than to determine the order of magnitude of H_x. In this case µ = 5,9742*10²⁴ [kg] is the Earth’s mass, r₀ = 1 AU = 1,496*10¹¹ [m] is the Sun-Earth mid-distance. With the above data, the minimum possible value of H_x is:

H_xmin2 ≥ 2,661962*10⁴⁰ [Js]      (80)

4.3. A Short Detour - Resonances of the Sun, and Other Stars

The resonances of the Sun - its natural frequency - if this physical property can be considered as a single characteristic, is the subject of numerous studies. In any case, it is barely sixty years since the so-called 300 s periodic oscillation became known. Since then, a vast literature has investigated numerous modes of oscillation (p, g, ...), and the causes of many of them also seem to be known. In any case, we can say that the highest amplitude is the first known ‘300 s’, i.e, ‘five-minute’, complex resonance - perhaps we are not making too great of a mistake in taking this value as the “natural frequency” of the Sun. This is perhaps also because the other, numerous modes of oscillation are even orders of magnitude smaller than this amplitude. First reported by Leighton R.B.et al. [10], and based on this by Christensen-Dalsgaard, J. [11]:

„…observations of oscillations of the solar surface were made by Leighton et al. (1962). They detected roughly periodic oscillations in local Doppler velocity with periods of around 300 s and a lifetime of at most a few periods. …. A confirmation of the initial detection of the oscillations was made by Evans and Michard (1962)…”

Similarly, according to Guglielmi A. V. et al. [12]

„..In the present paper we will focus on the oscillations of the photosphere with a period of 5 min, well known in helioseismology …”

In addition, it may be useful to consider a number of relevant contributions: Ulrich R.K. [13], Anderson, E. R et al. [14], Douglas Gough, D. [15], all report on the resonances of the Sun. According to the summary paper published by Garcia et al. [16], in our galaxy alone, there may be hundreds of millions of sun-type stars oscillating with quite similar p-mode resonance close to the above 300 s.

4.4. H_x Based on Measured Natural Frequency of the Sun

Based on the original definitions of quantum mechanics, the following relations can be written for a point of mass:

The Planck equation:

E = h*ν           (81)

The Einstein equation:

E = μ*c₂          (82)

As they imply, “...every particle of mass µ is, in a sense, a very precise ‘clock’ with a frequency ν proportional to its mass...” (Penrose [17]). This frequency is given by the above relation:

$$\mathrm{\nu }=\mathrm{\mu }{\displaystyle \frac{{\mathrm{c}}^2}{\mathrm{h}}}$$

(83)

where:

h = ℏ*2*π         (84)

$$\hslash =\mathrm{\mu }{\displaystyle \frac{{\mathrm{c}}^2}{2\mathrm{\pi }\mathrm{\nu }}}$$

(85)

In our case, based on the Sun’s eigenfrequency, we get the following equation:

$${\mathrm{H}}_{\mathrm{x}}=\mathrm{M}{\displaystyle \frac{{\mathrm{c}}^2}{2\mathrm{\pi }{\mathrm{\nu }}_{\mathrm{S}\mathrm{u}\mathrm{n}}}}$$

(86)

where c = 2,9978*10⁸ [m/s] the speed of light, ν_Sun $\cong$ 3,3 mHz = 0,0033 Hz = 0,0033 [1/s], the eigenfrequency of the Sun, M = 1,9891*10³⁰ [kg] the mass of the Sun. With this data:

$$\cong$$

$$\left[\mathrm{J}\mathrm{s}\right]$$

(87)

This value of H_x of 4.4 exceeds the theoretically calculated minimum values of H_xmin1, H_xmin2 in (72), (80) according to points 4.1 and 4.2.

5. Quantum Mechanical Model of Solar System-Like Systems

Almost every physical, quantum mechanical, and astronomical work since about the beginning of the 20th century mentions how the atomic structures are surprisingly similar, in many ways, to the ‘solar system-like’ structures. The ratio of central mass to orbiting masses, the ratio of distances between the central large mass and the orbiting smaller masses, etc. Then, almost all works state that the physical laws describing ‘solar system’ motions (such as the Newtonian model and general relativity) are of course, quite different from the relations describing atomic structures (relativistic quantum mechanics). Let us continue with this analogy. What would follow if we were to say that the solar system and its components are like many electrons orbiting a nucleus. Many works on quantum mechanics (and astronomy, cosmology) deal with the idea that quantum mechanical relations, ‘laws’, cannot be extended to the ‘macro-world’. The question may be what is the ‘macro-world’, where does it begin - how many atoms are the boundary, maybe a glass of milk, a big house, or a city, a continent, or let’s be brave: the Earth as a whole, maybe the whole solar system, but let’s go on: our Galaxy, or the Known Universe. In what follows, there is no need to ‘extend’ quantum mechanics - rather, let’s take a close look at the system under consideration, setting up the mathematical model, clarifying the boundary conditions, and applying all this to approximate reality as closely as possible. Let’s simply look at exactly what systems its laws apply to and under what conditions. In order to deal with solar system-like systems by quantum mechanics, i.e, for the analogy to work correctly, it is necessary that each element of the system be charged, identical particles, indistinguishable, with mass, spin, magnetic moment, the system being quantized. If all this is fulfilled, it would follow that the equations of motion of the atomic system can be applied to the solar system. An important premise of the work presented here is that solar system-like systems (possibly with individual actors Sun, Mercury, Venus, Earth, etc.) have charge. Measurements and models support the claim that they have a charge (Bailey [18], Neslusan [19]). Part of the model is that the central M mass has an opposite sign of charge. This ‘elementary charge’, which is a property of the constituent particles of the solar system, needs only to be stated here to exist (Dolezalek [20]).

The next question to be answered is whether we can consider members of solar-system-like systems as mass points. The answer is certainly yes, if we think on a very ‘large scale’ and try to observe them from a ‘terribly distant’ point. Even detection would be difficult, and from ‘very far away’, they could well be considered mass points of negligible size. This model is already quite similar to a legitimate application of the quantum mechanical approach. Solar system-like systems meet the requirements listed above. Each member of a solar system-like system has, beyond any doubt, mass, magnetic moment, and spin. Any source in the astronomical literature can support this. Immediately, questions and perhaps doubts may arise concerning some of the above points. Let us consider them in turn:

5.1. The Requirement of Indistinguishability

It is very easy to imagine that, viewed from a distance and sampled at very large intervals, all the motions in our solar system are merged, and the position and velocity of each mass cannot be measured separately. In other words, the basic conditions of quantum mechanics are met. If we look at several such systems from the outside, from a distance, simultaneously, sampled at very large intervals (by very large intervals we mean, for example, thousands, hundreds of thousands, millions, etc. of Earth years) the motion of the systems cannot be identified individually, we can only state laws about them as a whole, and these are, according to the conceptual framework of quantum mechanics: we have to talk about ‘identical’ particles, anointed cloud-like formations in space (and time), i.e. residence probabilities. Indistinguishability is apparently not immediately fulfilled, for example, when we are standing on the Earth and see how different, say, Jupiter is. But quantum mechanics does not ‘stand on the electron’ either. It examines the atom-electron with an ‘instrument’ (gigantic in size compared to individual atoms) built from atom-electrons. It determines probability distributions, and it sees an electron cloud. If we move away from the solar system, not so far, just a few hundred thousand light years, and extend the sampling frequency of the ‘measurement’ a little (not every minute, not every year, but much less frequently, with much larger time steps, even at intervals of several hundred thousand years), we immediately see an untraceable, indistinguishable ‘planetary cloud’. The time scale of sampling must be much larger than the orbital frequency of the ‘planetary cloud’. Like electrons. So the indistinguishability condition is already valid.

5.2. The Requirement of Charge

‘Charge’ is the only one of the features of the elements of a solar system-like system that is not immediately perceptible, not immediately visible, or a trivial characteristic. It can only be stated - Solar System-like systems have charge. This is supported by the measurements and facts presented in the cited literature. So then: suppose the Earth is a ‘big lumpy electron’. Ignore the fact that the Earth has countless complex features. What is ‘missing’, as far as we know, is the charge, or rather the property called charge, which is intrinsic to the (small) electron. That is, the Earth as a whole must have a charge to be treated as an ‘electron’. More specifically, the elements of solar system-like systems must have a property called ‘charge’. If it exists, then from this point of view, it is legitimate to treat, calculate, and interpret the whole system using a quantum mechanical model. Completely independently of the model discussed here, the charge of the individual solar system elements is known in the literature. For the moment, we refer only to the fact that the desired charge exists.

5.2. Charge Within the Solar System – Charge of the Sun

Sufficient data are available on the Sun’s charge. Studies of the solar corona have known theoretically for about a hundred years that the Sun (and stars in general) have a charge. In his article, Neslusan, referring to previous literature, also gives the magnitude of the charge as a function of solar (stellar) mass Q_r = 77.043*M_r , where Q_r is the global electrostatic charge of the star within a sphere of radius r, and M_r is the mass within a sphere of radius r. The formula is set up for an ideal star at rest - it can be accepted as an approximation. In any case, there is no doubt that the Sun (and other stars) have a charge.

5.3. Charge Within the Solar System – Charge of the Earth and the Planets

There are many measurements of the electrical properties of the individual actors and masses (mass points, planets) in the Solar System. The ionospheres of planets with atmospheres (e.g., Venus, Earth, etc.) have a property described as a ‘global electric circuit’ (Aplin [21,22]). There are many measurements of global electric circuits on Earth (Rycroft [23]) and Mars (Evtushenko [24]). The global electric circuit as a property can be extended to planets with dusty surfaces. The link with cosmic rays can be supported by measurements (Singh et al [25]). Of course, it may be a legitimate question whether this property can be considered as a ‘charge’ to the system ‘from the outside, at a distance’, using our modelling approach. The answer here is that yes, it is considered to be a charge. The cases outside the solar system are dealt with in the next chapter, but it should be noted that Aplin’s book referred to has a whole chapter on the possible ionization of exoplanets’ possible atmospheres. Our argument is strongly supported by the fact that the charge of the Sun is positive, while the charge of the Earth is negative. That is, they attract each other. The magnitude of this force, which may be very small, is not the primary issue for our model - the question is not how large the charge is, but whether it exists. The charge of the other planets can only be assumed to be negative for now. Convincing data on all this could be collected by measurements.

5.4. Charge Outside the Solar System – Planetary Nebulae

Planetary nebulae (PN) are perhaps the best suited to support the quantum mechanical analogy and model presented above from the point of view of measurements and observations. All that is currently known and worth knowing about planetary nebulae can be found in Kwok [26] in his thorough summary book. We can rely on this in the following. Among the PN properties covered in the book, there are two fundamental links to our quantum mechanical model: the ionization of PN systems, in our quantum mechanical terminology, the charge of the systems, and the morphology of PN systems. The most important facts that make PNs suitable for comparison and investigation in terms of quantum mechanics analogy and modelling are. According to classical (static) models of PNs, planetary nebulae are composed of two main components: the central star and the surrounding ionized gas nebula (see Kwok). Most PNs are in a fully ionized state. Of course, the material nebula surrounding the PN star has a much more complex composition than the simplified model above. If we consider the matter around the PN central star (or binary stars) as a whole: the matter cloud has a charge. With this property, PNs are measurement-proven evidence that stars and their surrounding matter in the system have a ‘charge’. This was the initial condition for using the quantum mechanics approach. That this is no exception among stars is confirmed by the following: nearly 95% of the stars in our Galaxy evolve as white dwarfs (WDs). Among these stars, a significant number (about 60%) evolve as Asymptotic Giant Branch (AGB) stars, evolving fast enough to ionize the surrounding envelope and be observed as PNs.

Another fundamental aspect that is important for us, and more precisely, the available measurement dataset, is the morphology of PNs. Several attempts have been made to classify the morphology of PNs. Among these classifications, the works of (Stanghellini, Manchado et al, Soker, Huarte-Espinoza, and Kwok [27,28,29,30,31,32,33,34,35,36,37]) are notable. According to the above-simplified classifications (Manchado et al [32]), the main morphologies, including frequency, are round (26%), elliptical (61%), bipolar-quadrupolar (13%), and quadrupolar (13%) PN systems. There are several physical-mathematical models in the literature to explain the diverse morphology of PN systems. There are some very successful models, with many important results being provided by the ISW (Interacting Stellar Winds) models of Kwok et al. and their modified and improved versions. The already cited Kwok et al. book, while offering a multifaceted answer to the morphological manifold, also poses a chapter-long question for us. The last of these questions, in summary, is: “...The morphological problem: what is the origin of this morphological diversity observed in planetary nebulae? The forms of PN appear symmetrical, but they take many different shapes...” There is no definitive, fully developed, unambiguous explanation as to why the PN manifold is so diverse and why it has such a variety of geometric shapes. The most striking is that the early diversity of morphology in the formation of PNs is already present during the pre-planetary life stage (PPN - Protoplanetary Nebulae). Since the PPN shows a similar morphological diversity as the mature PN, this suggests that a shape-determining mechanism must be at work early in the evolutionary phase. The quantum mechanical model can provide a new perspective on morphological diversity. The conceptual framework, physical models, and mathematics of relativistic quantum mechanics have been applied to quantum mechanical modelling [38]. However, the models and calculations based on non-relativistic quantum mechanics are sufficiently accurate for speeds much lower than the speed of light (c) and provide results that hardly differ from those of relativistic quantum mechanics - for example, the solutions of the radial probability density distributions of the hydrogen atom using the modified Dirac equation hardly differ from the results based on the Schrödinger equation. This implies that the nature of the radial probability density distributions in three-dimensional (3D) representations can be well approximated by non-relativistic models. We compared these non-relativistic three-dimensional probability density distributions, which are much easier to compute and represent, with the morphological diversity of planetary nebulae. Each quantum mechanical 3D state was matched to a morphological PN shape. The 3D probability density distributions show a surprisingly good similarity with the observed morphological shapes of PN.

5.5. Charge Outside the Solar System – Compact Charged Stars

The fact that stars are charged can also be confirmed by the stars classified as “compact charged stars”. It suffices to mention a few selected examples from the literature ([39,40,41,42,43]). Ray and colleagues in their 2003 paper [41] report the following:

„…We conclude that in order to see any appreciable effect on the phenomenology of compact stars, electrical fields have to be huge (> 10²¹ V/m), which implies that the total electric charge is Q > 10²⁰ Coulomb…”

Jasim and colleagues in 2021 [42] also provide numerical evidence for the possible magnitude of the charge:

„…It is 10²⁰ Coulomb for each these stars..”

5.6. Estimated, Computable Charges of the Sun and Planets

Values of charges within the solar system which can be approximated based on the analogy. If we accept the comparable relationships based on the quantum mechanical analogy, then according to ‘Bohr’s magneton’ formula: ${\mathrm{\mu }}_{\mathrm{B}}={\displaystyle \frac{\mathrm{e}}{{\mathrm{m}}_{\mathrm{e}}}}{\displaystyle \frac{\mathrm{\hslash }}{2}}$ and applying the analogy, the relevant correlation: ${\mathrm{\mu }}_{\mathrm{x}}={\displaystyle \frac{{\mathrm{e}}_{\mathrm{x}}}{{\mathrm{M}}_{\mathrm{x}}}}{\displaystyle \frac{{\mathrm{H}}_{\mathrm{x}}}{2}}$ where H_x is the new constant derived above, e_x is the unknown charge being sought, M_x is the mass value according to the analogy, and µ_x is the magnetic moment. Magnetic moments are in many cases known from astronomical data, so we can summarize the values that can be calculated in this way in the following table:

Name	Mass Mx [kg]	Magnetic moment µx [Am2]	Calculated charge ex [C]
Sun	1,989E+30	3,000E+30	1,385E+12
Mercury	3,302E+23	3,800E+19	2,911E-06
Venus	4,869E+24	6,500E+19	7,343E-05
Earth	5,974E+24	8,000E+22	1,109E-01
Mars	6,419E+23	(0,000E+00)	(0,000E+00)
Jupiter	1,899E+27	1,627E+27	7,169E+05
Saturn	5,684E+26	4,650E+25	6,132E+03

In the case of the Sun, the value of 1.3851*10¹² [C] should be evaluated based on astronomical data. A basis for comparison can be the estimated charge of compact stars according to the scientific literature, which is approximately 10²⁰ [C]; compared to this, a value on many order of magnitude smaller is possible.

In the case of the Earth, the value of 1.11*10^-1 [C] should be evaluated based on available data. According to the scientific literature, the estimated charge of the Earth is near to zero [C], compared to which the calculated value seems to hold.

The data for the other members of the solar system cannot be verified. In the case of Mars, it is known that it may have had a magnetic moment of approximately 10²⁰ in the past, which would correspond to a charge of 1.5*10^-4 [C].

It is interesting for us to compare the estimated charge values with the forces between the Sun and the planet, and to compare these with the force according to gravitational effects. The values of the calculated charges assumed in this way are not conclusive data. At the same time, they do not refute the validity of the analogy.

5.7. Estimated, Computable Force Due to Sun’s Charge

Let’s try to estimate, based on the data above, how much of the Sun’s presumed charge might affect the Earth. A highly simplified (Newtonian) model is way sufficient here and now for comparison and to illustrate the orders of magnitude:

The force acting on the planet from the Sun’s charge ${\mathrm{F}}_{\mathrm{x}}=\mathrm{k}{\displaystyle \frac{{\mathrm{q}}_{\mathrm{S}\mathrm{u}\mathrm{n}}\mathrm{*}{\mathrm{q}}_{\mathrm{x}}}{{{\mathrm{r}}_{\mathrm{x}}}^2}}$, where k=8,988*10⁹ [Nm²/C²]. The force acting on the planet due to gravitational effect, approximated (only the mass of the Sun is taken into account): ${\mathrm{F}}_{\mathrm{G}}=\mathrm{G}{\displaystyle \frac{{\mathrm{M}}_{\mathrm{S}\mathrm{u}\mathrm{n}}\mathrm{*}{\mathrm{m}}_{\mathrm{x}}}{{{\mathrm{r}}_{\mathrm{x}}}^2}}$, where G=6,674*10^-11 [Nm²/kg²]

As a rough estimate, based on the average distance between the Sun and Earth, where r_x = 5,791*10¹⁰ [m]

Estimated force Fx = 6,166*10^-2 [N]

Estimated force F_G = 3,544*10²² [N]

According to the data above, the forces resulting from (presumed) charges are many orders of magnitude smaller than gravitational effects (in the case of Earth, this is 24 orders of magnitude!). All this corresponds to observed reality – there are no ‘unknown forces’ being measured anywhere. It seems almost unimaginable that such differences in magnitude could be detected by measurement. Yet it would be important to determine how to measure the electrostatic force effect exerted by the Sun on a charged terrestrial body.

5.8. Generating Charge - Magnitude

First, let’s consider how to create a charge on a terrestrial object of non-extreme size, and how this can be done. There are excellent solutions for this; among the best known and most widely used is the Van de Graaff generator. The magnitude of the charge can be an important factor. With a Van de Graaff generator, a charge of a certain magnitude can be easily generated on the surface of a sphere in a laboratory-level setting: The sphere should have a diameter of approximately 15–30 cm.

The magnitude of the electric field $\mathrm{E}={\displaystyle \frac{1}{4\mathrm{\pi }{\mathrm{\epsilon }}_0}}{\displaystyle \frac{\mathrm{Q}}{{\mathrm{r}}^2}}$ [V/m]

where Q charge [C], ε₀ = 8,854*10^-12 [F/m], r the radius of the sphere = 0,01 [m]

Let’s determine the maximum electric field strength that can be achieved in air without discharge (for a sphere with a diameter of approximately, say, 20 cm), given that the permittivity of air is approximately 3*10⁶ [V/m]. Let’s take a value lower than this, say approx. E = 2*10⁶ [V/m]. Using these data, based on the magnitude of E above:

$\mathrm{Q}=\mathrm{E}\mathrm{*}\mathrm{\pi }\mathrm{*}{\mathrm{\epsilon }}_0\mathrm{*}{\mathrm{r}}^2$ [C] = 2*10⁶*4*π*8,854*10^-12*0,01² [C]

Q ≈ 2,225*10^-8 [C]

(At the same time, an electric field strength of up to 10⁸ V/m can be generated in a vacuum, and by increasing the radius of the sphere, a much higher charge can be generated).

5.9. The Force Between the Sun and the Sphere with the Above Charge

The approximated force between the Sun and the above charged sphere:

${\mathrm{F}}_{\mathrm{x}}=\mathrm{k}{\displaystyle \frac{{\mathrm{q}}_{\mathrm{S}\mathrm{u}\mathrm{n}}\mathrm{*}{\mathrm{q}}_{\mathrm{x}}}{{{\mathrm{r}}_{\mathrm{x}}}^2}}$, with k=8,988*10⁹ [Nm²/C²]

${\mathrm{F}}_{\mathrm{x}}=\mathrm{8,988}\mathrm{*}{10}^9{\displaystyle \frac{\mathrm{1,385}\mathrm{*}{10}^{12}\mathrm{*}\mathrm{2,225}\mathrm{*}{10}^{-8}}{{\left(\mathrm{1,496}\mathrm{*}{10}^{11}\right)}^2}}$F_x = 1,2376*10^-8 [N]

This force could not have been detected in any way previously, nor could it have played a role anywhere. The question is whether it is possible to measure the effect of this force of approximately 10⁻⁸ [N]. The answer to this question may be obtained by using a modified Cavendish torsion balance, or a modified Eötvös torsion balance, with their rotations magnified by mirrors and lasers. A torsion balance is capable of detecting changes in g on the order of 10⁻⁹. By modifying these torsion balances appropriately, a force of this magnitude can, in principle, be measured. In our case, compared to the uncharged initial state of the sphere, we would need to measure and interpret the rotation of a sphere charged using, for example, the Van de Graaff method while suspended on a torsion wire. If the force effect can be detected by measurement, this could serve as evidence for the Sun’s charge, its magnitude, and the validity of the theory determining the charge.

6. Requirement of Quantization

So far, there has been no discussion of whether quantized orbits exist in the Solar System or in Solar System-like systems. We know one such system quite well, our own solar system, for which we have known for a few hundred years that masses do not orbit just anywhere. The regularity of the radial distribution of the planets has been known for centuries. Many theoretical approximations have attempted to explain it. The fundamental reasons for the regularity of the planetary distribution, known as the ’Titius-Bode Law’, are not clearly known. The fact that within the solar system, within the sphere bounded by the Oort cloud, the masses (planets, minor planetary belt, etc.) (which can be understood as mass points) form a kind of geometrically well-defined system is beyond dispute. The question for centuries has been whether this is just a coincidence, and what makes it so. Everyone is familiar with the geometric series of Titius (1766) and Bode (1772). Nieto’s thorough and intriguing summary (1992) [44] of possible physical models can certainly provide possible, not excludable, explanations - he presents a myriad of existing models.

At the same time, it may be possible to find a modeling state in which solar system-like systems can be discussed using quantum mechanical tools. Graner and Dubrulle, in their double publication (1993) [45] and [46], show that all previous interpretations of the above geometric regularity are based on a kind of scale invariance. Numerous such theoretical models can be constructed. Their second publication offers the possibility to “build your own law”. As they show, the diversity of theories can be explained by “scale invariance”. The contradictions and possibilities of other models are outlined in [47]. Among the possibilities, the work of Nottale (1996 - 1997) [48,49], who suggests the possibility of quantizing the solar system and even the universe on the basis of scale relativity, stands out.

Of the myriad theoretical possibilities, none contradicts the assumption suggested by the quantum mechanical model presented in this chapter that the radial probability density distribution can be explained. Concerning the quantum mechanical approach, special mention should be made of the work of Jehle (1938) [50]. Jehle shows the quantum mechanical interpretability of stellar systems based on Schrödinger’s wave functions of quantum mechanics. He also attempts to derive the radial distribution of masses for the solar system. He concludes that Planck’s ℏ has “nothing to do” with his theory (“bemerken wir...dass...diese Theorie nichts mit Planck-schen Wirkungsquantum zu tun hat...”). This statement is given by the relativistic quantum mechanical derivations presented in this chapter without any prior assumption, by itself, supported by mathematical means (based on H_x values). In his derivations of the theory, Jehle proves that in any given system of stars, a kind of indeterminacy relation (Δx Δv ≥ σ) holds, where σ is interpreted as σ ≈ M_Sternsystem, (where M_Sternsystem, in this case, is the total mass of the solar system, which is roughly 2*10³³. Based on his derivations, he believes that the magnitude of the new factor is at least σ≈ M/8π, which does not contradict the relations obtained for the minimum value of H_x derived here). At the end of the paper, he refers to the fact that Dirac’s interpretation of relativistic quantum mechanics is a deeper interpretation of quantum mechanics “...die Tiefere Bedeutung der Wellenmechanik...”. In this paper, this is the starting point for the model presented.

The radial distribution of planets in the Solar System can be modelled using quantum mechanics as a radial probability density function. However, a selection rule is needed, supported by appropriate physical arguments. To compare the model numerically with the planetary distribution, a “selection rule” (a special “Pauli principle”) corresponding to the chapters of [51,57] would be needed to model the interpretation of the radial probability distributions of solar system-like systems. Noting all this, the correspondence between the model and the real planetary distribution is hopeful.

The rotation and magnetic axes of planets in the Solar System are another possible argument. In quantum mechanical atomic systems, the number and properties of the electrons on each electron shell are governed by special laws (Pauli’s principle). The innermost shell can have two electrons, whose spins must be opposite. Within the solar system, Mercury and Venus are the two inner planets. Their rotation (spin) is opposite. Venus is the only planet with a retrograde rotation. This is surprising, even according to astronomical sources, and there is no satisfactory explanation. The explanation is simple by analogy: this is the only possible spin state of the second planet. In any case, it is striking that, of the two inner planets (Mercury and Venus), Venus has the opposite spin as the only one in the solar system. In addition, no two planets have the same spin and magnetic dipole moment vectors [51,57]. Within the Solar System, the inclination of the rotation axis of the planets concerning the ecliptic is diverse - there is currently no satisfactory explanation for this diversity. If the quantum mechanical analogy is valid, then the expectation for planets, based on Pauli’s law, would be that no two planets can be in the same ‘state’. This can be decided partly by the spin states (different angles of rotation) and partly by the magnetic moment states. If we look at the planets of the Solar System with the data currently known [52,53,54,55,56], the law seems to hold.

7. Summary

The key statements of the presented model are the following:

• Solar system-like systems can be described by the physical models and mathematical tools of relativistic quantum mechanics. The basic relativistic equations by analogy are valid in a weak gravitational field, the gravitational potential and the electric potential exist independently and simultaneously.
• An approximate value for H_x for the solar system can be determined from calculations and measurements.
• The charge of the Sun can be calculated using the analogy.

Quantum mechanics is valid, but not in ‘a slightly larger’ macro-world, but in a world that fully satisfies the basic assumptions of the original quantum mechanics. The quantum mechanical model based on the modified Dirac equation has no scale. That is, it is valid in all cases that satisfy the initial assumptions. For example, in weak gravitational fields, in solar system-like systems. The quantum mechanical analogy, i.e, the model described here, does not contradict existing physical-mathematical models. It simply approaches the problem from a different direction.