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Preprints of the Keldysh Institute of Applied Mathematics, 2011, 047, 24 pp. (Mi ipmp153)  
Autorotation motion of a satellite in a low circular orbit

S. A. Mirer, I. V. Prilepskiy
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Abstract: Attitude dynamics of a satellite in a low circular orbit is analyzed taking into account the rotating aerodynamic torque resulting due to special installation of solar panels. The existence of the stationary rotations in the orbital reference frame is studied. The number of these rotations is analyzed analytically and numerically. For several specific cases, stability analysis is performed. For the asymptotically stable rotations, the speed of response is estimated.
Keywords: atellite, aerodynamic torque, autoro tation, stationary rotation, stability.
Document Type: Preprint
Language: Russian
Citation: S. A. Mirer, I. V. Prilepskiy, “Autorotation motion of a satellite in a low circular orbit”, Keldysh Institute preprints, 2011, 047, 24 pp.
Citation in format AMSBIB
\Bibitem{MirPri11}
\by S.~A.~Mirer, I.~V.~Prilepskiy
\paper Autorotation motion of a satellite in a low circular orbit
\jour Keldysh Institute preprints
\yr 2011
\papernumber 047
\totalpages 24
\mathnet{http://mi.mathnet.ru/ipmp153}
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    		Препринты Института прикладной математики им. М. В. Келдыша РАН
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