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Subhalo or Future–Mass Projection? A Like-for-Like Pulsar-Acceleration Test with an Explicit Real-Space FMP Kernel, Quantitative PPN↔kpc Bridge, and Uncertainty-Aware Population Rates

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16 September 2025

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17 September 2025

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Abstract
Binary-pulsar accelerations have been interpreted as evidence for a local ∼ 107 M⊙ subhalo. We strengthen the like-for-like confrontation with Future–Mass Projection (FMP) by: (i) deriving a closed, numerically stable real-space kernel Γϵ(r) from ϵ(k) = ϵ0 (1+k2/k2 0 )−1 W (k) with W (k) = 1 − e−(k/kw )2 , including exact erf/erfc forms, asymptotics, and a monotonicity proof; (ii) computing a quantitative Solar-System map ϵSS(ϵ0, k0, kw) with (|β − 1|, | ˙G/G|) for concrete feasibility points; (iii) providing analytic bounds that link the required kpc-scale acceleration to PPN safety and the forecast baryon budget; (iv) specifying a reproducible Π → Meff → alos pipeline (ROI, hyperpriors, figure/table slots); (v) refactoring detection rates with a 68% band from (ρDM, fsub, ∆ ln M ). We retain the published compact/NFW subhalo evidences as benchmarks and define ready-to-populate outputs (log-evidence table, corner plots, vector-geometry comparison) for the FMP runs under the same GP likelihood.
Keywords: 
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1. Data, Geometry, and Baseline Likelihood

The benchmark pulsar analysis reports a subhalo-like solution at ( X , Y , Z ) ( 7.5 , 0.38 , 0.21 ) kpc with Bayes factors 20 –40 (compact vs. smooth) and 30 (NFW with r s 0.1  kpc, c 30 ), and a preferred mass ( 2.5 6.2 ) × 10 7 M ; other sightlines provide upper limits. We adopt the same sky geometry, priors, and noise (white jitter per pulsar + shared red-noise GP with amplitude A RN , slope γ RN ). For a compact perturber,
a los , i sub = G M sub | r i r sub | 3 ( r i r sub ) · n ^ i ,
with the NFW variant using ( r s , c ) . The marginalized GP likelihood ln L = 1 2 ( d m ) C 1 ( d m ) 1 2 ln | C | N 2 ln 2 π (with C = N white + GP ) is used identically for subhalo and FMP.

2. FMP in 3D: Explicit Kernel, Field, and Projection

We parameterize the response in Fourier space
ϵ ( k ) = ϵ 0 1 1 + k 2 / k 0 2 W ( k ) , W ( k ) = 1 e ( k / k w ) 2 .
The added potential obeys Δ Φ ( k ) = 4 π G ρ b ( k ) ϵ ( k ) / k 2 , giving a real-space acceleration
a FMP ( r ) = d 3 r ρ b ( r ) Γ ϵ ( | r r | ) , Γ ϵ ( r ) = F 1 ϵ ( k ) k 2 ( r ) .
Closed form (Yukawa minus Gaussian-smoothed Yukawa). Using 1 k 2 ( 1 + k 2 / k 0 2 ) = 1 k 2 1 k 2 + k 0 2 and the isotropic pairs F 1 [ 1 / k 2 ] = 1 / ( 4 π r ) and F 1 [ 1 / ( k 2 + k 0 2 ) ] = e k 0 r / ( 4 π r ) , the W 1 kernel is Γ ϵ ( W = 1 ) ( r ) = ϵ 0 ( 4 π r ) 1 e k 0 r ( 4 π r ) 1 . For general W ( k ) , e ( k / k w ) 2 maps to a real-space Gaussian G σ ( r ) e r 2 / ( 2 σ 2 ) with σ = 2 / k w , hence
Γ ϵ ( r ) = ϵ 0 1 4 π r e k 0 r 4 π r ϵ 0 1 4 π r e k 0 r 4 π r G σ ( r ) ,
with the Ewald form for the Yukawa–Gaussian convolution:
e k 0 r 4 π r G σ = e k 0 2 σ 2 8 π r e k 0 r erfc r 2 σ k 0 σ e + k 0 r erfc r 2 σ + k 0 σ , 1 4 π r G σ = 1 4 π r erf r 2 σ .
Monotonicity: For ϵ 0 , k 0 , k w > 0 , Γ ϵ ( r ) is positive and strictly decreasing for r > 0 (difference of completely monotone kernels, smoothing preserves complete monotonicity); thus no spurious oscillations in a FMP .
Vector projection (like-for-like).
a los , i FMP = a FMP ( r i ) · n ^ i = G d 3 r ρ b ( r ) Γ ϵ ( | r i r | ) ( r i r ) · n ^ i | r i r | ,
with Γ ϵ ( r ) = d Γ ϵ / d r .

3. Solar-System Safety ↔ Kpc Strength: Quantitative Bridge

Define ϵ SS = ϵ ( k AU ) = ϵ 0 [ 1 + k AU 2 / k 0 2 ] 1 [ 1 e ( k AU / k w ) 2 ] with k AU = 1 / AU in kpc units (so k AU 2.06 × 10 8 kpc 1 ). Post-Newtonian scalings: | β 1 | C β ϵ SS 2 (with C β 3 ), | G ˙ / G | H 0 ϵ SS . For representative feasibility points:
Table 1. PPN mapping for concrete FMP points ( H 0 7.2 × 10 11 yr 1 ).
Table 1. PPN mapping for concrete FMP points ( H 0 7.2 × 10 11 yr 1 ).
Case ϵ 0 k 0 1 [kpc] k w 1 [kpc] ϵ SS | β 1 | ( C β = 3 ) | G ˙ / G | [ yr 1 ]
A 0.05 0.6 0.4 3.3 × 10 18 3.3 × 10 35 2.4 × 10 28
B 0.03 1.0 0.6 7.1 × 10 19 1.5 × 10 36 5.1 × 10 29
C 0.08 0.4 0.3 4.0 × 10 18 4.8 × 10 35 2.9 × 10 28

Analytic Bounds Linking Kpc Amplitude to PPN Safety

For an ROI volume V with baryon density ρ b , triangle inequality on (4) yields
| a los , i FMP | G V d 3 r ρ b ( r ) | Γ ϵ ( | r i r | ) | .
Using the closed form for Γ ϵ and assuming a conservative spherical ROI of radius R and total forecast mass M b ( forecast ) , we obtain two useful bounds:
G ϵ 0 M b ( forecast ) R 2 1 e ( R k w ) 2 1 1 + R k 0 lower ( central clump ) | a FMP | G ϵ 0 M b ( forecast ) R 2 upper ( point - like ) ,
which bracket the exact value for any anisotropy in ρ b . Thus, for | a | 10 9 cm s 2 at R = 0.4 –1 kpc and M b ( forecast ) [ 3 × 10 8 , 2 × 10 9 ] M , the required ϵ 0 lies in the 10 2 10 1 range provided ( k 0 1 , k w 1 ) 0.3 –1 kpc. The table above shows that such choices remain vastly PPN-safe due to the W ( k AU ) suppression.

4. Forecast Operator Π M eff a los  (Operational)

We employ a linear-Gaussian state-space model for s = ( ρ HI , ρ H 2 , ρ ) :
s t + Δ t = A s t + u t + η t , η t N ( 0 , Q ) , y t = H s t + ϵ t , ϵ t N ( 0 , R ) .
ROI: centred on the preferred sky region of the detection set; Modalities:i cubes (tens pc voxels), CO(1–0) mosaics for H 2 , 3D dust, Gaia DR3 kinematics. Hyperpriors:  Q log-uniform in [ 10 4 , 10 1 ] of median voxel-mass per Δ t , R from survey noise; A encodes mild relaxation + shear/compression from spiral templates. The smoother yields p [ s t + τ | I t ] , then
M b ( forecast ) ( t + τ ) = V ( ρ HI + ρ H 2 + ρ ) d 3 x , M eff = 0 K ( τ ) M b ( forecast ) ( t + τ ) d τ ,
and a los , i FMP through (4). To insert: (i) posterior mean & 1 σ map of M b ( forecast ) for the ROI; (ii) histogram of M eff with mean/CI; (iii) propagated a los , i FMP with uncertainties.

5. Vector Geometry: Per-Pulsar Comparison

To insert: a table with ( l , b ) , a los data ± σ , a los sub , a los FMP for all pulsars, and a rose diagram of acceleration directions (data vs. subhalo vs. FMP) to quantify directional coherence.

6. Detection Probabilities with Uncertainty Bands

We correct the local density to 0.3 GeV cm 3 = ( 7.9 ± 2.6 ) × 10 6 M kpc 3 , use d N / d M = A M 2 with Δ ln M = 1 , and obtain
n ( M ) 0.0868 f sub M 10 7 M 1 kpc 3 , P 1 = 4 π 3 n Δ r obs 3 f sub M 1 / 2 a 3 / 2 .
We plot P 1 = 1 ( 1 P 1 ) 5 with a 68 % band propagated from ρ DM [ 5.3 , 10.5 ] × 10 6 , f sub [ 0.01 , 0.05 ] , and ln ( M max / M min ) [ 7 , 10 ] ; assumptions M = 10 7 M , a = 10 9 cm s 2 .
Figure 1. Five-try detection probability with corrected ρ DM and a 68 % band (from ρ DM , f sub , Δ ln M ). Assumptions: M = 10 7 M , a = 10 9 cm s 2 .
Figure 1. Five-try detection probability with corrected ρ DM and a 68 % band (from ρ DM , f sub , Δ ln M ). Assumptions: M = 10 7 M , a = 10 9 cm s 2 .
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7. Model Comparison Outputs (to Be Populated After the Run)

Benchmarks (quoted): compact/NFW best fits and Bayes factors for the detection set (as in the published analysis).
FMP (same likelihood/priors): insert (i) log Z table (Smooth/Compact/NFW/FMP, with ±SE), (ii) corner plots for ( ϵ 0 , k 0 , k w , τ F ) , (iii) per-pulsar vector table and rose diagram. Use Savage–Dickey at ϵ 0 0 for FMP vs. smooth.

8. Conclusions

With explicit field kernels, a computed PPN map, analytic bounds to connect kpc amplitude and Solar-System safety, and an operational Π M eff a los path, FMP becomes a quantitatively testable like-for-like alternative to a local subhalo in pulsar accelerations. The remaining step is mechanical: run the shared GP pipeline and insert the FMP evidences/posteriors and geometry tables into the provided slots.

Reproducibility and Priors

FMP priors:  ϵ 0 [ 0 , 0.08 ] , k 0 1 [ 0.1 , 1.5 ]  kpc, k w 1 [ 0.2 , 2 ]  kpc, τ F [ 0.1 , 1 ]  Gyr; enforce ϵ SS 10 5 , λ 0 10 3  AU.
Repo layout: /pulsar/ (GP likelihood & evidence), /fmp/ (kernel Γ ϵ , projector), /forecast/ (Kalman smoother), /figs/ (PPN, bounds, P 1 ).

Notation and Unit Bridges

k 0 1 / λ 0 ; 1 AU = 4.848 × 10 9 kpc k AU 2.06 × 10 8 kpc 1 .
0.3 GeV cm 3 = ( 7.9 ± 2.6 ) × 10 6 M kpc 3 (derivation in Appendix B).

Appendix A. Real-Space Kernel Details and Validation

From (3),
Γ ϵ ( r ) = ϵ 0 1 erf r 2 σ 4 π r ϵ 0 e k 0 2 σ 2 8 π r e k 0 r erfc r 2 σ k 0 σ e + k 0 r erfc r 2 σ + k 0 σ .
Asymptotics:  Γ ϵ ( r ) ϵ 0 ( 4 π r ) 1 [ ( r / ( 2 σ ) ) / π + O ( r 3 ) ] as r 0 ; and Γ ϵ ( r ) ϵ 0 ( 4 π r ) [ 1 e k 0 r ] ϵ 0 ( 4 π r ) [ 1 O ( e r 2 / 2 σ 2 ) ] as r .
Validation: 1D Hankel transform of ϵ ( k ) / k 2 vs. the closed form agrees to machine precision over grids in ( ϵ 0 , k 0 , k w ) ; recipe and tolerance listed in the code notes.

Appendix B. Detection-Rate Derivation with Units

With d N / d M = A M 2 and Δ ln M = 1 , n ( M ) = dex ( d N / d M ) d M A / M . Using ρ DM = M ( d N / d M ) d M = A ln ( M max / M min ) , we normalize A = ρ DM / ln ( M max / M min ) and obtain n ( M ) ρ DM / [ M ln ( M max / M min ) ] . The single-try probability in a sphere of radius Δ r obs is P 1 = 4 π 3 n Δ r obs 3 , yielding P 1 f sub M 1 / 2 a 3 / 2 after inserting the observational reach Δ r obs from the pulsar sensitivity formula.

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