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Active inertial magnetic attitude of a satellite in gravitational field
V. I. Penkov, D. S. Roldugin
Abstract:
Active magnetic attitude control system providing arbitrary inertial attitude of the satellite is considered. Control and gravitational torques are taken into account. Planar motion is considered for the periodical solutions analysis. Stability is analyzed using the Floquet theory, optimal algorithm parameters are chosen. Overall gravity effect is assessed.
Keywords:
magnetic attitude control system, three-axis stabilization, gravitational torque.
Citation:
V. I. Penkov, D. S. Roldugin, “Active inertial magnetic attitude of a satellite in gravitational field”, Keldysh Institute preprints, 2018, 163, 18 pp.
Linking options:
https://www.mathnet.ru/eng/ipmp2522 https://www.mathnet.ru/eng/ipmp/y2018/p163
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