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- W2755749355 abstract "The dynamics of the high-speed vehicle (HSV) is partially or completely unknown because of various reasons, such as modeling errors, in-flight failure, and external disturbances. In this paper, a global stability robust fuzzy controller is designed to control the flight F-16 with uncertain perturbation. For the desired H ∞ output-feedback controllers, a necessary and sufficient condition of quadratic stability is derived with the well-established results of the Lyapunov stability theory and nonnegative matrix. The controllers not only guarantee the global asymptotically stability of the resultant closed-loop system with external disturbance and parameter perturbation, but also have a desired H ∞ performance in a large flight envelop (LFE)." @default.
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- W2755749355 date "2017-03-25" @default.
- W2755749355 modified "2023-09-29" @default.
- W2755749355 title "High Speed Aircraft Robust Fuzzy Controller Design Based on H ∞ Performance" @default.
- W2755749355 doi "https://doi.org/10.11989/jest.1674-862x.5102615" @default.
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