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- W3043581495 abstract "The stabilization of the relative equilibrium of a satellite in a circular orbit is considered. The satellite is equipped with a magnetic orientation system. A new analytic approach to the study of this problem is proposed. It is shown that the linearized system of equations of motion belongs to a special class of the linear time-varying control systems that are reducible to the higher-order time invariant ones. Based on the obtained time invariant system, controllability is studied, and stabilization algorithms are constructed. The results of numerical simulation confirm the effectiveness of the proposed methodology." @default.
- W3043581495 created "2020-07-23" @default.
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- W3043581495 date "2020-06-01" @default.
- W3043581495 modified "2023-09-23" @default.
- W3043581495 title "Controllability of the satellite stabilized by magnetic torques" @default.
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- W3043581495 doi "https://doi.org/10.1109/stab49150.2020.9140719" @default.
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