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Magnetic attitude control in orbital frame. Vector of finite rotation control method
V. I. Penkov, M. Yu. Ovchinnikov, D. S. Roldugin
Abstract:
Attitude motion of a satellite equipped with an active magnetic attitude control system is considered. Two control approaches using the finite rotation vector are proposed. Control parameters are adjusted for big robust control authority and small but realistic control values. Numerical simulation is carried out to demonstrate the control capabilities.
Keywords:
magnetic attitude control system, vector of finite rotation.
Citation:
V. I. Penkov, M. Yu. Ovchinnikov, D. S. Roldugin, “Magnetic attitude control in orbital frame. Vector of finite rotation control method”, Keldysh Institute preprints, 2018, 007, 21 pp.
Linking options:
https://www.mathnet.ru/eng/ipmp2368 https://www.mathnet.ru/eng/ipmp/y2018/p7
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Statistics & downloads: |
Abstract page: | 218 | Full-text PDF : | 78 | References: | 26 |
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