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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
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.
flexible element, normal mode, model verification
Publication language: russian,  pages: 19
Research direction:
Theoretical and applied problems of mechanics
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About authors:
  • Nuralieva Anna Borisovna, RAS
  • Tkachev Stepan Sergeevich, RAS