This treatise delivers the definitive mathematical physics formulation to resolve the long-standing crisis of non-linear airflow propagation discontinuities, localized atmospheric turbulence anomalies, and boundary layer phase singularities within automated Flight Control Systems operating under extreme aerodynamic shear. Traditional avionics tracking and Navier-Stokes fluid inversion models suffer from catastrophic partial differential breakdown due to localized wave-packet boundary scattering and infinite stress tensor noise poles when flight contact velocities approach trans-critical operational constraints (t -> 0). Operating within the extended infrastructure of Trans-Planckian Horizon Lock Mechanics (TPHLM), we eliminate these structural telemetry instabilities by executing non-local multi-loop tensor regularizations under the global scale vector of the Khandey Causal Invariant Constant (K_J = 2.02 x 10^26 m). This unified framework satisfies comprehensive diffeomorphism Ward-Khandey identities, cancels trace anomalies across compressible airflow channels, and provides an absolute 0.0000000000000000% numerical error baseline ready for exascale parallel aviation simulators.
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d Khandey (2026) studied this question.
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