H∞ output tracking control for flight control systems with time-varying delay

被引:0
|
作者
Zhang Yingxin [1 ]
Wang Qing [1 ]
Dong Chaoyang [2 ]
Jiang Yifan [1 ]
机构
[1] School of Automation Science and Electrical Engineering,Beihang University
[2] School of Aeronautic Science and Engineering,Beihang University
基金
中国国家自然科学基金;
关键词
Discrete time control systems; Flight control systems; H∞ output tracking; Time-varying delay; Uncertainty;
D O I
暂无
中图分类号
V249.1 [飞行控制];
学科分类号
081105 ;
摘要
For flight control systems with time-varying delay,an H∞output tracking controller is proposed.The controller is designed for the discrete-time state-space model of general aircraft to reduce the effects of uncertainties of the mathematical model,external disturbances,and bounded time-varying delay.It is assumed that the feedback-control loop is closed by the communication network,and the network-based control architecture induces time-delays in the feedback information.Suppose that the time delay has both an upper bound and a lower bound.By using the Lyapunov-Krasovskii function and the linear matrix inequality(LMI),the delay-dependent stability criterion is derived for the time-delay system.Based on the criterion,a state-feedback H∞output tracking controller for systems with norm-bounded uncertainties and time-varying delay is presented.The control scheme is applied to the high incidence research model(HIRM),which shows the effectiveness of the proposed approach.
引用
收藏
页码:1251 / 1258
页数:8
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