Adaptive backstepping control for air-breathing hypersonic vehicle subject to mismatched uncertainties

被引:16
|
作者
Yu, Chaojun [1 ]
Jiang, Ju [1 ]
Zhen, Ziyang [1 ]
Bhatia, Ajeet Kumar [1 ]
Wang, Shuo [1 ]
机构
[1] Nanjing Univ Aeronaut & Astronaut, Coll Automat Engn, Nanjing 211106, Peoples R China
基金
中国国家自然科学基金;
关键词
Air-breathing hypersonic vehicle (AHV); Mismatched uncertainties; Coordinate transformation; Backstepping control; Adaptive control; Projection operator; SLIDING-MODE CONTROL; DYNAMIC SURFACE CONTROL; FAULT-TOLERANT CONTROL; TRACKING CONTROL; CONTROL DESIGN; NONLINEAR-SYSTEMS; CONTROL SCHEME; APPROXIMATION;
D O I
10.1016/j.ast.2020.106244
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This paper studies the tracking control problem of the air-breathing hypersonic vehicle (AHV) subject to mismatched uncertainties. A novel model transformation is proposed for AHV with uncertain parameters, to address the unavailable states problem of conventional model transformation. Then, a novel adaptive backstepping control method is proposed for a class of nonlinear system with mismatched uncertainties, and a projection operator is designed to avoid the singular problem. The adaptive controller guarantees asymptotical command tracking, instead of uniformly ultimate boundness (UUB), for the closed-loop uncertain system. Then, the proposed control scheme is directly applied to the design of flight controller based on the transformed model. Lastly, a detailed simulation is conducted to demonstrate the efficiency and superiority of the proposed method. (c) 2020 Elsevier Masson SAS. All rights reserved.
引用
收藏
页数:19
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