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KIAM Preprint № 26, Moscow, 2015
Authors: Ovchinnikov M. Y., Hao-Chi Chang, Mirer S. A., Roldugin D. S., Tkachev S. S.
Dynamical model of a satellite with controllable solar array
Abstract:
Satellite with 3DOF solar panel is considered. Satellite is a rigid bodies while solar panel consists of three parts connected by 1 DOF hinges. The work is aimed at the satellite-panel system attitude dynamical model construction.
Keywords:
complex structure, solar panel, 3DOF hinge, equations of motion
Publication language: english,  pages: 19
Research direction:
Theoretical and applied problems of mechanics
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About authors:
  • Ovchinnikov Michael Yurievich,  ovchinni@keldysh.ru,  orcid.org/0000-0003-2377-4490,  KIAM RAS
  • Hao-Chi Chang,  National Space Organization, Taiwan
  • Mirer S. A.,  mirer@keldysh.ru,  KIAM RAS
  • Roldugin Dmitry Sergeevich,  rolduginds@gmail.com,  orcid.org/0000-0002-9616-0994,  KIAM RAS
  • Tkachev Stepan Sergeevich,  stevens_l@mail.ru,  orcid.org/0000-0002-1971-7867,  KIAM RAS
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