arXiv · 1507.06963
Controllability of Spacecraft Using Only Magnetic Torques
Abstract
Spacecraft attitude control using only magnetic torques is a time-varying system. Many designs were proposed using LQR and H-infinity formulations. The existence of the solutions depends on the controllability of the linear time-varying systems which has not been established. In this paper, we will derive the conditions of the controllability for this linear time-varying systems.
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Yaguang Yang. 2015-07-24. Controllability of Spacecraft Using Only Magnetic Torques. https://doi.org/10.1109/taes.2015.150520
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