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• W2748700541 abstract "This paper presents a robust fuzzy tracking controller for position and attitude control, and for vibration suppression in a flexible spacecraft. The robust fuzzy controller guarantees H <sub xmlns:mml=http://www.w3.org/1998/Math/MathML xmlns:xlink=http://www.w3.org/1999/xlink>∞</sub> tracking control performance while satisfying the actuators' amplitude constraints. The design problem of the fuzzy tracking controller is formulated in terms of linear matrix inequalities. The stability, performance, and robustness of the proposed fuzzy controller are examined and compared with a baseline nonlinear controller such as the model-reference adaptive controller with σ-modification via numerical simulations." @default.
• W2748700541 created "2017-08-31" @default.
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• W2748700541 date "2018-02-01" @default.
• W2748700541 modified "2023-09-23" @default.
• W2748700541 title "Robust Fuzzy Tracking Control of Flexible Spacecraft via a T–S Fuzzy Model" @default.
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• W2748700541 doi "https://doi.org/10.1109/taes.2017.2740078" @default.
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