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KIAM Preprint  83, Moscow, 2013
Authors: Ovchinnikov M. Y., Tkachev S. S., Roldugin D. S.
Attitude control system failure cases response using operational actuators
Abstract:
Typical magneto-gyroscopic attitude control system failures are considered, Chibis-M microsatellite is used as an example. Mission recovery for each case is investigated. It is impossible to upload new attitude control algorithms on board. Gravitational boom is an auxiliary component of the attitude control system element and it is considered separately.
Keywords:
magneto-gyroscopic attitude control system, gravitational boom
Publication language: russian,  pages: 29
Research direction:
Theoretical and applied problems of mechanics
Russian source text:
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About authors:
  • Ovchinnikov Michael Yurievich,  KIAM RAS
  • Tkachev Stepan Sergeevich,  orcid.org/0000-0002-1971-7867KIAM RAS
  • Roldugin Dmitry Sergeevich,  orcid.org/0000-0002-9616-0994KIAM RAS