On Stability of Sattellite's Elliptical Orbit Motion for Cylindrical Precession of Lunar Type Resonance

Abstract

Stability of satellites elliptical orbit motion in the case of the cylindrical precession at
Lunar type resonance is under investigation. Stability regions at first approximation have
been obtained in the space of parameters of the problem (inertial parameter and eccentricity).
Nonlinear analysis is carried out in these regions. Analytical and numerical methods are used.