Output feedback sliding mode control with finite time trajectory tracking performance for the hypersonic vehicles

被引:0
|
作者
Li, Mingxing [1 ]
Jia, Yingmin [1 ]
机构
[1] Beihang Univ BUAA, Sch Automat Sci & Elect Engn, Ctr Informat & Control, Res Div 7, Beijing 100191, Peoples R China
关键词
Hypersonic vehicle; Finite time control; Sliding mode control;
D O I
暂无
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
In this paper, the finite time trajectory tracking method is established for hypersonic vehicles. A new quasi-linear parameter varying model is proposed and a finite time controller is designed by the sliding mode method of output feedback. The matching conditions of disturbances and uncertainties are satisfied naturally which ensures the established control method has very excellent robustness and practicability. Simulations show that very accurately tracking trajectory results are obtained while the velocity and altitude are varying in large flight envelops.
引用
收藏
页码:9460 / 9465
页数:6
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