Published April 26, 2022
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Attitude Regulation With Bounded Control in the Presence of Large Disturbances With Bounded Moving Average
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The attitude regulation problem with bounded control for a class of satellites in the presence of large disturbances, with bounded moving average, is solved using a Lyapunov-like design. The analysis and design approaches are introduced in the case in which the underlying system is an integrator and are then applied to the satellite attitude regulation problem. The performance of the resulting closed-loop systems are studied in detail and it is shown that trajectories are ultimately bounded despite the effect of the persistent disturbance. Simulation results on a model of a small satellite subject to large, but bounded in moving average, disturbances are presented.
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2022 IEEE. Personal use of this material is permitted. Permission from IEEE must be obtained for all other uses, in any current or future media, including reprinting/republishing this material for advertising or promotional purposes, creating new collective works, for resale or redistribution to servers or lists, or reuse of any copyrighted component of this work in other works. A. Li, A. Astolfi, and M. Liu, "Attitude Regulation With Bounded Control in the Presence of Large Disturbances With Bounded Moving Average," IEEE/CAA Journal of Automatica Sinica, vol. 9, no. 5, pp. 834-846, May 2022, doi: 10.1109/JAS.2022.105557.
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