Optimum parameters of a gravitational-gyroscopic satellite orientation system

Details Optimum parameters of a gravitational-gyroscopic satellite orientation system Optimum parameters of a gravitational-gyroscopic satellite orientation system

May 1975

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1975kosis..13..311s&link_type=abstract

Kosmicheskie Issledovaniia, vol. 13, May-June 1975, p. 311-321. In Russian.

Physics

Equations Of Motion, Gravity Gradient Satellites, Gyroscopic Stability, Oscillation Dampers, Satellite Orientation, Time Optimal Control, Asymptotic Methods, Axisymmetric Bodies, Circular Orbits, Motion Stability, Precession, Satellite Attitude Control

Scientific paper

General equations of motion are derived for a satellite with two gyroscopes using the theory of gyroscopic precession. Conditions are obtained for the zero-position equilibrium of a satellite in a circular orbit, and the stability of such equilibrium is analyzed. Values of the gyroscope parameters are determined which yield maximum response from the orientation system.

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