轨道稳定性常数及新天体力学理论体系

Description

Abstract

This achievement represents a major original innovation in the fields of fundamental physics and celestial mechanics, constructing a logically consistent, self-contained, and fully verifiable new theoretical system of celestial mechanics. Centered on an original orbital stability constant, it introduces an innovative method for calculating centripetal force in orbital motion, alongside formulas for orbit verification and satellite orbit design. It establishes an orbital stability determination mechanism that unifies single-body orbital motion and two-body motion, and provides the first rigorous derivation of the law of universal gravitation and Kepler's third law, addressing a core theoretical gap in classical mechanics that has persisted for over three hundred years. The system has been fully validated through numerical closed-loop verification using measured data from the Sun-Earth system, Earth-Moon system, near-Earth space stations, and the Sirius AB binary star system. It can be directly applied to scenarios including satellite orbit design, on-orbit status inspection, orbital stability determination, planetary orbit analysis, and high-precision orbit control, offering both significant theoretical breakthroughs and practical engineering value.