Abstract Dynamics of an axisymmetric gyrostat satellite moving in the central Newtonian force field along a circular orbit is investigated. All equilibrium positions of the gyrostat satellite in the orbital coordinate system are determined, and the sufficient stability conditions of equilibrium positions are derived.
Dynamics of an axisymmetric gyrostat satellite under the action of gravitational moment
Cosmic Research ; 48 , 2
2010
Article (Journal)
English
BKL: | 50.93 Weltraumforschung / 39.00 Astronomie: Allgemeines / 55.60 Raumfahrttechnik | |
Local classification TIB: | 770/3520/8000 |
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