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• W4310257961 endingPage "105392" @default.
• W4310257961 startingPage "105392" @default.
• W4310257961 abstract "This paper presents a dual-mode attitude controller for air-breathing hypersonic vehicles, which strategically switches between cruising and maneuvering modes. Each mode designs a neural inversion to partly decouple attitude dynamics having actuator transient behaviors and magnitude-rate constraints. As a direct benefit, the inverse algorithm for the most-frequently-used cruising mode becomes low-complexity. Aiming at decoupled attitude channels, an enhanced inner-loop controller is proposed to accommodate uncertain modeling, imprecise decoupling and nonzero allocating. In especial, its self-initializing mechanism eliminates fluctuations aroused by mode changes. The dual-mode attitude controller is further integrated with guidance and scramjet control modules to form a general six-degrees-of-freedom control system." @default.
• W4310257961 created "2022-11-30" @default.
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• W4310257961 date "2023-02-01" @default.
• W4310257961 modified "2023-10-17" @default.
• W4310257961 title "Dual-mode control of hypersonic vehicles" @default.
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• W4310257961 doi "https://doi.org/10.1016/j.conengprac.2022.105392" @default.
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