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Preprints of the Keldysh Institute of Applied Mathematics, 2011, 021, 28 pp.
(Mi ipmp127)
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This article is cited in 1 scientific paper (total in 1 paper)
Active magnetic attitude control system of a satellite equipped with a flywheel
M. Yu. Ovchinnikov, D. S. Roldugin M. V. Keldysh Institute for Applied Mathematics, Russian Academy of Sciences
Abstract:
Attitude motion of a satellite equipped with a single flywheel and active magnetic attitude control system is considered. Time-response of the system in a transient mode with respect to the orbit inclination is studied. Comparison with the system consisting of magnetic coils only is conducted. Small steady-state motion near the gravitational orientation is considered. Accuracy and time-response is studied. An algorithm of arbitrary but given orientation in the orbital plane is proposed and studied. Numerical analysis is carried out.
Keywords:
active magnetic control, flywheel, averaged geomagnetic field model, time-response.
Citation:
M. Yu. Ovchinnikov, D. S. Roldugin, “Active magnetic attitude control system of a satellite equipped with a flywheel”, Keldysh Institute preprints, 2011, 021, 28 pp.
Linking options:
https://www.mathnet.ru/eng/ipmp127 https://www.mathnet.ru/eng/ipmp/y2011/p21
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Abstract page: | 179 | Full-text PDF : | 71 | References: | 41 |
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