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Preprints of the Keldysh Institute of Applied Mathematics, 2015, 058, 20 pp.
(Mi ipmp2020)
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This article is cited in 2 scientific papers (total in 2 papers)
Equations of motion for a satellite with flexible parts
S. S. Tkachev, D. S. Roldugin, M. Yu. Ovchinnikov
Abstract:
The mathematical model for a satellite with flexible parts is developed. The eigen modes are used for the flexible parts motion description. Linearized equations are derived.
Keywords:
satellite, flexible elements, motion equations.
Citation:
S. S. Tkachev, D. S. Roldugin, M. Yu. Ovchinnikov, “Equations of motion for a satellite with flexible parts”, Keldysh Institute preprints, 2015, 058, 20 pp.
Linking options:
https://www.mathnet.ru/eng/ipmp2020 https://www.mathnet.ru/eng/ipmp/y2015/p58
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