Active robust control of uncertainty and flexibility suppression for air-breathing hypersonic vehicles

被引:39
作者
Pu, Zhiqiang [1 ]
Yuan, Ruyi [1 ]
Tan, Xiangmin [1 ]
Yi, Jianqiang [1 ]
机构
[1] Chinese Acad Sci, Inst Automat, Beijing 100190, Peoples R China
基金
中国国家自然科学基金;
关键词
Hypersonic vehicle; Uncertainty; Flexibility; Extended state observer; Notch filter; TRACKING CONTROL; DESIGN;
D O I
10.1016/j.ast.2015.01.028
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Inevitable uncertainties and cross couplings between rigid and flexible modes pose huge challenges to control system design for flexible air-breathing hypersonic vehicles. This paper addresses an active robust control scheme that can simultaneously suppress diverse uncertainties and flexible modes using active approaches rather than inherent system robustness. Frequency-domain analysis is conducted to investigate the cross couplings. A novel conclusion lies in that the most significant cross couplings exist between the flexible modes and the rigid-body phugoid modes, followed by the altitude mode. Based on the analysis, a robust control scheme is proposed which consists of a stabilizing control frame and two active control techniques: a nonlinear extended state observer (ESO) and a notch filter. The ESO estimates diverse uncertainties to form a compensation law, and the notch filter is integrated to prevent the flexible modes from being excited by some specific high-frequency signals coming from the ESO estimated values. Thus, both uncertainties and flexible modes can be simultaneously suppressed. A Lyapunov-based stability analysis is conducted for the overall closed-loop system. At last, several representative simulations are conducted to demonstrate the advantages of the proposed active control scheme. (C) 2015 Elsevier Masson SAS. All rights reserved.
引用
收藏
页码:429 / 441
页数:13
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