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• W2924827986 abstract "In this paper, the problem of output feedback robust H∞ control for spacecraft rendezvous system with parameter uncertainties, disturbances and input saturation is investigated. Firstly, a full-order state observer is designed to reconstruct the full state information, whose gain matrix can be obtained by solving the linear matrix inequality (LMI). Subsequently, by combining the parametric Riccati equation approach and gain scheduled technique, an observer-based robust output feedback gain scheduled control scheme is proposed, which can make full use of the limited control capacity and improve the control performance by scheduling the control gain parameter increasingly. Rigorous stability analyses are shown that the designed discrete gain scheduled controller has faster convergence performance and better robustness than static gain controller. Finally, the performance and advantage of the proposed gain scheduled control scheme are demonstrated by numerical simulation." @default.
• W2924827986 created "2019-04-01" @default.
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• W2924827986 creator A5064291165 @default.
• W2924827986 date "2019-05-01" @default.
• W2924827986 modified "2023-10-13" @default.
• W2924827986 title "Output feedback robust H∞ control for spacecraft rendezvous system subject to input saturation: A gain scheduled approach" @default.
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• W2924827986 doi "https://doi.org/10.1016/j.jfranklin.2018.12.023" @default.
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