Fuzzy Disturbance Observer-Based Fixed-Time Sliding Mode Control for Hypersonic Morphing Vehicles With Uncertainties

被引:19
作者
Chen, Haolan [1 ]
Wang, Peng [1 ]
Tang, Guojian [1 ]
机构
[1] Natl Univ Def Technol, Coll Aerosp Sci & Engn, Changsha 410073, Peoples R China
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); CONVERGENCE TIME; AIRCRAFT; SYSTEMS; DESIGN;
D O I
10.1109/TAES.2022.3227886
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
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.
引用
收藏
页码:3521 / 3530
页数:10
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