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

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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.

About the authors

T E Churkina

Moscow Aviation Institute

Кафедра теоретической механики; Московский авиационный институт; Moscow Aviation Institute


Copyright (c) 2009 Чуркина Т.Е.

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