The results of flight tests of an attitude control system for the Chibis-M microsatellite
Autor: | Danil Ivanov, M. Yu. Ovchinnikov, S. O. Karpenko, Dmitry Sergeevich Roldugin, N. A. Ivlev, Stepan Sergeevich Tkachev |
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Rok vydání: | 2014 |
Předmět: | |
Zdroj: | Cosmic Research. 52:205-215 |
ISSN: | 1608-3075 0010-9525 |
DOI: | 10.1134/s0010952514020038 |
Popis: | The attitude control system of the Chibis-M microsatellite is described. Results of flight experiments on damping the initial angular velocity (made using magnetorquers) are considered, as well as stabilization in the orbital referece frame, and orientation of solar arrays toward the Sun using reaction wheels. The operation of algorithms of satellite attitude determination on sunlit and shadow segments of the orbit is also under study. The general logic of operation of the attitude control system in automatic mode is presented and discussed. |
Databáze: | OpenAIRE |
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