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Preprints of the Keldysh Institute of Applied Mathematics, 2015, 047, 20 pp.
(Mi ipmp2009)
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Three-axis satellite stabilization using only magnetorquers and magnetometer
D. S. Ivanov, M. Yu. Ovchinnikov, V. I. Penkov, D. S. Roldugin, D. M. Doronin, A. V. Ovchinnikov
Abstract:
Attitude motion of a satellite equipped with magnetic control system is considered. System comprises of three mutually orthogonal magnetorquers and one three-axis magnetometer. Satellite is stabilized in orbital reference frame in equilibrium position unstable in gravitational field. Two control strategies are presented. Three-axis attitude is shown to be achievable. Accuracy in presence of disturbing torques and inertia moments uncertainty is assessed.
Keywords:
magnetic attitude control system, three-axis magnetometer, three-axis attitude, Kalman filter.
Citation:
D. S. Ivanov, M. Yu. Ovchinnikov, V. I. Penkov, D. S. Roldugin, D. M. Doronin, A. V. Ovchinnikov, “Three-axis satellite stabilization using only magnetorquers and magnetometer”, Keldysh Institute preprints, 2015, 047, 20 pp.
Linking options:
https://www.mathnet.ru/eng/ipmp2009 https://www.mathnet.ru/eng/ipmp/y2015/p47
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Statistics & downloads: |
Abstract page: | 265 | Full-text PDF : | 130 | References: | 41 |
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