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JOURNALS // Preprints of the Keldysh Institute of Applied Mathematics // Archive

Keldysh Institute preprints, 2014 013, 24 pp. (Mi ipmp1865)

This article is cited in 1 paper

Dynamical model of a satellite with 2DOF solar panel

M. Yu. Ovchinnikov, Chang Hao-Chi, S. A. Mirer, D. S. Roldugin, S. S. Tkachev


Abstract: Satellite with 2DOF solar panel is considered. The panel hinge consists of a motor capable of panel attitude control. Satellite and solar panel are rigid bodies both. The work is aimed at the satellite-panel system attitude dynamical model construction.

Keywords: complex structure, solar panel, 2DOF hinge, equations of motion.

Language: English



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