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KIAM Preprint № 61, Moscow, 2015
Authors: Nuralieva A. B., Tkachev S. S.
Mathematical model for a satellite with flexible 1DOF hinged solar panel
Abstract:
Mathematical model of a satellite with flexible 1DOF hinged solar panel is considered. Nonlinear and linearized equations are derived. Model verification using first integrals of motion and normal modes is carried out.
Keywords:
flexible element, normal mode, model verification
Publication language: russian,  pages: 19
Research direction:
Theoretical and applied problems of mechanics
Russian source text:
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