Tracking control of air-breathing hypersonic vehicles with non-affine dynamics via improved neural back-stepping design

被引:80
作者
Bu, Xiangwei [1 ]
He, Guangjun [1 ]
Wang, Ke [1 ]
机构
[1] Air Force Engn Univ, Air & Missile Def Coll, Xian 710051, Shaanxi, Peoples R China
基金
中国国家自然科学基金;
关键词
Air-breathing hypersonic vehicle (AHV); Non-affine dynamics; Improved back-stepping; Neural approximation; OUTPUT-FEEDBACK; FLIGHT VEHICLE; ADAPTIVE-CONTROL; CONTROL SCHEME; UNCERTAINTY;
D O I
10.1016/j.isatra.2018.02.010
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
This study considers the design of a new back-stepping control approach for air-breathing hypersonic vehicle (AHV) non-affine models via neural approximation. The AHV's non-affine dynamics is decomposed into velocity subsystem and altitude subsystem to be controlled separately, and robust adaptive tracking control laws are developed using improved back-stepping designs. Neural networks are applied to estimate the unknown non-affine dynamics, which guarantees the addressed controllers with satisfactory robustness against uncertainties. In comparison with the existing control methodologies, the special contributions are that the non-affine issue is handled by constructing two low-pass filters based on model transformations, and virtual controllers are treated as intermediate variables such that they aren't needed for back-stepping designs any more. Lyapunov techniques are employed to show the uniformly ultimately boundedness of all closed-loop signals. Finally, simulation results are presented to verify the tracking performance and superiorities of the investigated control strategy. (C) 2018 ISA. Published by Elsevier Ltd. All rights reserved.
引用
收藏
页码:88 / 100
页数:13
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