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KIAM Preprint № 13, Moscow, 2014
Authors: Ovchinnikov M. Y., Hao-Chi Chang, Mirer S. A., Roldugin D. S., Tkachev S. S.
Dynamical model of a satellite with 2DOF solar panel
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
Publication language: english,  pages: 24
Research direction:
Theoretical and applied problems of mechanics
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About authors:
  • Ovchinnikov Michael Yurievich,  orcid.org/0000-0003-2377-4490KIAM RAS
  • Hao-Chi Chang,  ,  National space organization (NSPO, Taiwan)
  • Mirer S. A.,  KIAM RAS
  • Roldugin Dmitry Sergeevich,  orcid.org/0000-0002-9616-0994KIAM RAS
  • Tkachev Stepan Sergeevich,  orcid.org/0000-0002-1971-7867KIAM RAS