Sarychev, V.A. (1965) Dynamics of a Satellite Gravitational Stabilization with Consideration of Atmospheric Resistance. Proceedings of the Eleventh International Congress of Applied Mechanics Munich (Germany), 1964, 429-435.

has been cited by the following article:

• TITLE: Relative Equilibria of a Satellite Moving in an Elliptic Orbit Subjected to Gravitational and Aerodynamic Torques

  AUTHORS: Kumari Ranjana

  KEYWORDS: Satellite; Gravitational and Aerodynamic Torques; Equilibria; Condition of Stability

  JOURNAL NAME: International Journal of Astronomy and Astrophysics, Vol.4 No.1, March 21, 2014

  ABSTRACT: Here we consider the attitude motion of a satellite, subjected to gravitational and aerodynamic torques in an elliptic orbit. The determination of orientation of equilibrium points has been discussed. It is found that they coincide with those for the circular case as studied by Sarychev and others in the works [1]-[3] and besides we have aimed at the sufficient condition for stability in the sense of Lyapunov.