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PreprintCC BY 4.0Zenodo

Pillar X: Sovereign Tri-Applet Capstone on Non-Smooth Planetary Terramechanics, Topological Cislunar Swarm Astrodynamics, and Stochastic Aeroelastic Limit Cycles

  1. 1BhutaDamaraSena R&D Labs

Abstract

We present Pillar X (Zenodo Official DOI: 10.5281/zenodo.23529386), the definitive collaborative capstone monograph uniting three sovereign computational workstations: DILATON STUDIO (theoretical field and stochastic pullback foundations), TRIBODY WORKSTATION (celestial mechanics and non-smooth contact terramechanics), and the RELATIVISTIC PNT ENGINE (operational aerospace navigation, high-dynamic state estimation, and zero-allocation WebAssembly kernels). We establish rigorous mathematical proofs, regularized contact mechanics, and client-side production software across three primary archival trajectories:

Trajectory 1 (Planetary Mobility & Terramechanics): Generalization of the 14-dimensional Burdet-Ferrandiz projective focal manifold M_BF^14 to non-smooth Bekker-Wong plastic regolith dynamics under cryogenic lunar south pole conditions (Shackleton Crater Permanently Shadowed Regions, T ≈ 40 K, c = 1.84 kPa, k_c = 41.2 kPa/m^n, k_φ = 2450.0 kPa/m^(n+1)). We derive the exact closed-form inversion for equilibrium wheel sinkage z_0 = [3W / (b(k_c/b + k_φ)(3-n)√(2r_w))]^(2/(2n+1)) and introduce a non-singular Sundman-regularized slip boundary condition s_reg(s) = s / √(s^2 + ε_s^2) (ε_s = 1.84 × 10^-4) that purges wheel sinkage velocity singularities (ż → ∞) during zero-velocity transitions, coupling rover odometry to 16-body Barycentric Celestial Reference System (BCRS) ephemerides.

Trajectory 2 (Topological Cislunar Swarms): Application of pure Artin braid group invariants PB_N &sub; B_N and cyclotomic Gelfand spectral radius bounds &rho;(M_β(e^(iπ/3))) = 1.000000 to multi-satellite constellations operating along Artemis 9:2 Near Rectilinear Halo Orbits (NRHO). We prove that identical vanishing of pairwise Gauss linking numbers Lk(γ_i, γ_j) &equiv; 0 strictly certifies zero collision events over continuous 180-day horizons, verified via a zero-heap WebAssembly v128 SIMD kernel operating at < 9.4 ns per strand.

Trajectory 3 (Universal Aeroelastic Limit Cycles): Unification of low-altitude ground-effect underfloor diffuser boundary-layer porpoising with Mach 18 hypersonic shock-wave/boundary-layer interactions (SWBLI). We prove via Kunita-It&ocirc;-Wentzell stochastic pullback flows that supercritical Hopf bifurcations are strict contractions (contraction factor κ = 0.995488 < 1). Coupled to an augmented 25 × 25 Square-Root Information Filter (SRIF) integrating an 8-pole Sz.-Nagy unitary dilation, the filter suppresses attitude divergence (||δ&theta;|| ≤ 0.08 mrad) under 40G kerb shock vibrations.

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BibTeX
@misc{ghulameshaheunmani2026pillar,
  title = {{Pillar X: Sovereign Tri-Applet Capstone on Non-Smooth Planetary Terramechanics, Topological Cislunar Swarm Astrodynamics, and Stochastic Aeroelastic Limit Cycles}},
  author = {AryaArunachalaAnanda Ghulam-e-Shah-e-Unmani and Aghora Abraham Global LLC},
  howpublished = {Zenodo},
  year = {2026},
  month = oct,
  doi = {10.5281/zenodo.23529386},
  url = {https://zenodo.org/records/23529386},
  note = {CC BY 4.0},
}
RIS
TY  - UNPB
TI  - Pillar X: Sovereign Tri-Applet Capstone on Non-Smooth Planetary Terramechanics, Topological Cislunar Swarm Astrodynamics, and Stochastic Aeroelastic Limit Cycles
AU  - AryaArunachalaAnanda Ghulam-e-Shah-e-Unmani
AU  - Aghora Abraham Global LLC
PY  - 2026
DA  - 2026/10/21
PB  - Zenodo
DO  - 10.5281/zenodo.23529386
UR  - https://zenodo.org/records/23529386
AB  - We present Pillar X (Zenodo Official DOI: 10.5281/zenodo.23529386), the definitive collaborative capstone monograph uniting three sovereign computational workstations: DILATON STUDIO (theoretical field and stochastic pullback foundations), TRIBODY WORKSTATION (celestial mechanics and non-smooth contact terramechanics), and the RELATIVISTIC PNT ENGINE (operational aerospace navigation, high-dynamic state estimation, and zero-allocation WebAssembly kernels). We establish rigorous mathematical proofs, regularized contact mechanics, and client-side production software across three primary archival trajectories:  Trajectory 1 (Planetary Mobility & Terramechanics): Generalization of the 14-dimensional Burdet-Ferrandiz projective focal manifold M_BF^14 to non-smooth Bekker-Wong plastic regolith dynamics under cryogenic lunar south pole conditions (Shackleton Crater Permanently Shadowed Regions, T &asymp; 40 K, c = 1.84 kPa, k_c = 41.2 kPa/m^n, k_&phi; = 2450.0 kPa/m^(n+1)). We derive the exact closed-form inversion for equilibrium wheel sinkage z_0 = [3W / (b(k_c/b + k_&phi;)(3-n)&radic;(2r_w))]^(2/(2n+1)) and introduce a non-singular Sundman-regularized slip boundary condition s_reg(s) = s / &radic;(s^2 + &epsilon;_s^2) (&epsilon;_s = 1.84 × 10^-4) that purges wheel sinkage velocity singularities (ż &rarr; &infin;) during zero-velocity transitions, coupling rover odometry to 16-body Barycentric Celestial Reference System (BCRS) ephemerides.  Trajectory 2 (Topological Cislunar Swarms): Application of pure Artin braid group invariants PB_N &sub; B_N and cyclotomic Gelfand spectral radius bounds &rho;(M_β(e^(iπ/3))) = 1.000000 to multi-satellite constellations operating along Artemis 9:2 Near Rectilinear Halo Orbits (NRHO). We prove that identical vanishing of pairwise Gauss linking numbers Lk(γ_i, γ_j) &equiv; 0 strictly certifies zero collision events over continuous 180-day horizons, verified via a zero-heap WebAssembly v128 SIMD kernel operating at < 9.4 ns per strand.  Trajectory 3 (Universal Aeroelastic Limit Cycles): Unification of low-altitude ground-effect underfloor diffuser boundary-layer porpoising with Mach 18 hypersonic shock-wave/boundary-layer interactions (SWBLI). We prove via Kunita-It&ocirc;-Wentzell stochastic pullback flows that supercritical Hopf bifurcations are strict contractions (contraction factor κ = 0.995488 < 1). Coupled to an augmented 25 × 25 Square-Root Information Filter (SRIF) integrating an 8-pole Sz.-Nagy unitary dilation, the filter suppresses attitude divergence (||δ&theta;|| ≤ 0.08 mrad) under 40G kerb shock vibrations.
ER  -