The dynamical structure of the MEO region: long-term stability, chaos, and transport

TL;DR

This paper investigates the complex resonances and chaotic dynamics in the MEO region affecting navigation satellites, using analytical models and stability maps to understand long-term stability and chaos.

Contribution

It introduces analytical and semi-analytical models to accurately characterize resonant interactions and chaos in the MEO region, aiding satellite disposal strategies.

Findings

Chaotic regions are extensive near navigation satellite inclinations.

Transition from stable to chaotic regimes occurs between 3 and 5 Earth radii.

Many inclined, nearly circular orbits exhibit strong chaos with unpredictable dynamics.

Abstract

It has long been suspected that the Global Navigation Satellite Systems exist in a background of complex resonances and chaotic motion; yet, the precise dynamical character of these phenomena remains elusive. Recent studies have shown that the occurrence and nature of the resonances driving these dynamics depend chiefly on the frequencies of nodal and apsidal precession and the rate of regression of the Moon's nodes. Woven throughout the inclination and eccentricity phase space is an exceedingly complicated web-like structure of lunisolar secular resonances, which become particularly dense near the inclinations of the navigation satellite orbits. A clear picture of the physical significance of these resonances is of considerable practical interest for the design of disposal strategies for the four constellations. Here we present analytical and semi-analytical models that accurately reflect the true nature of the resonant interactions, and trace the topological organization of the manifolds on which the chaotic motions take place. We present an atlas of FLI stability maps, showing the extent of the chaotic regions of the phase space, computed through a hierarchy of more realistic, and more complicated, models, and compare the chaotic zones in these charts with the analytical estimation of the width of the chaotic layers from the heuristic Chirikov resonance-overlap criterion. As the semi-major axis of the satellite is receding, we observe a transition from stable Nekhoroshev-like structures at three Earth radii, where regular orbits dominate, to a Chirikov regime where resonances overlap at five Earth radii. From a numerical estimation of the Lyapunov times, we find that many of the inclined, nearly circular orbits of the navigation satellites are strongly chaotic and that their dynamics are unpredictable on decadal timescales.