Geodesic
Influence of the variable aerodynamic moment on satellite attitude motion
Izvestiya of Saratov University. Mathematics. Mechanics. Informatics, Tome 11 (2011) no. 3, pp. 67-74.

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Attitude motion of a rigid body in the plane of a circular orbit under gravitational and aerodynamic moments is considered. The mode of the motion of a satellite gravitational stabilization when its long axis moves in the vicinity of a local vertical is investigated. Allowance of variations in the atmosphere density at a satellite orbital motion and in the aerodynamic moment coefficient depending on its orientation to an approach flow is included in the aerodynamic moment model. An analytical solution of a small oscillations equation is obtained, and it is shown that the variability of the aerodynamic moment may have a pronounced effect on the accuracy of the satellite stabilization. 
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V. S. Aslanov; A. V. Pirozhenko; A. V. Kislov; A. I. Maslova. Influence of the variable aerodynamic moment on satellite attitude motion. Izvestiya of Saratov University. Mathematics. Mechanics. Informatics, Tome 11 (2011) no. 3, pp. 67-74. http://geodesic.mathdoc.fr/item/ISU_2011_11_3_a9/

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