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Preprints of the Keldysh Institute of Applied Mathematics, 2015, 026, 19 pp. (Mi ipmp1989)  
Dynamical model of a satellite with controllable solar array

M. Yu. Ovchinnikov, Hao-Chi Chang, S. A. Mirer, S. S. Tkachev, D. S. Roldugin
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Abstract: Satellite with 3DOF solar panel is considered. Satellite is a rigid body while solar panel consists of three parts connected by 1 DOF hinges. The work is aimed at the satellite-panel system attitude dynamical model construction.
Keywords: complex structure, solar panel, 3DOF hinge, equations of motion.
Document Type: Preprint
Language: English
Citation: M. Yu. Ovchinnikov, Hao-Chi Chang, S. A. Mirer, S. S. Tkachev, D. S. Roldugin, “Dynamical model of a satellite with controllable solar array”, Keldysh Institute preprints, 2015, 026, 19 pp.
Citation in format AMSBIB
\Bibitem{OvcChaMir15}
\by M.~Yu.~Ovchinnikov, Hao-Chi~Chang, S.~A.~Mirer, S.~S.~Tkachev, D.~S.~Roldugin
\paper Dynamical model of a satellite with controllable solar array
\jour Keldysh Institute preprints
\yr 2015
\papernumber 026
\totalpages 19
\mathnet{http://mi.mathnet.ru/ipmp1989}
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    		Препринты Института прикладной математики им. М. В. Келдыша РАН
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