期刊
IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS
卷 59, 期 4, 页码 3521-3530出版社
IEEE-INST ELECTRICAL ELECTRONICS ENGINEERS INC
DOI: 10.1109/TAES.2022.3227886
关键词
Aerodynamics; Disturbance observers; Vehicle dynamics; Uncertainty; Control systems; Convergence; Stability criteria; Fixed-time stability; fuzzy disturbance observer (FDO); homogeneity theory; hypersonic morphing vehicles (HMVs); sliding mode control (SMC)
This work focuses on attitude control problem for hypersonic morphing vehicles (HMVs) with uncertainties. A disturbance observer with fuzzy logic system (FLS) is proposed to enhance the robustness. The control system degenerates into an autonomous system, and the closed-loop fixed-time stability is guaranteed via Lyapunov synthesis and homogeneity theory.
This work focuses on the attitude control problem for hypersonic morphing vehicles (HMVs) with uncertainties. A span-morphing HMV model is first established with lumped disturbances. Based on fixed-time technique, a disturbance observer with fuzzy logic system (FLS) is proposed to enhance the robustness by estimating the unmodeled dynamics and external disturbances in fixed settling time. The multivariable fixed-time sliding mode manifold is applied to the transformed control system, which guarantees a direct control input design from attitude command and decent tracking performance. Then, the control system degenerates into an autonomous system, and the closed-loop fixed-time stability is ensured via Lyapunov synthesis and homogeneity theory. Finally, simulation results are presented to demonstrate the effectiveness of the proposed control scheme.
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