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Preprints of the Keldysh Institute of Applied Mathematics, 2014, 013, 24 pp.
(Mi ipmp1865)
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This article is cited in 1 scientific paper (total 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.
Citation:
M. Yu. Ovchinnikov, Chang Hao-Chi, S. A. Mirer, D. S. Roldugin, S. S. Tkachev, “Dynamical model of a satellite with 2DOF solar panel”, Keldysh Institute preprints, 2014, 013, 24 pp.
Linking options:
https://www.mathnet.ru/eng/ipmp1865 https://www.mathnet.ru/eng/ipmp/y2014/p13
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Statistics & downloads: |
Abstract page: | 173 | Full-text PDF : | 63 | References: | 35 |
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