Super-twisting sliding mode control based on Lyapunov analysis for the cursing flight of hypersonic vehicles

被引:0
作者
Mu, Chaoxu [1 ]
Sun, Changyin [2 ]
Qian, Chengshan [2 ]
Zhang, Ruimin [2 ]
机构
[1] Tianjin Univ, Dept Elect Engn & Automat, Tianjin 300072, Peoples R China
[2] Southeast Univ, Sch Automat, Nanjing 210096, Peoples R China
来源
2013 10TH IEEE INTERNATIONAL CONFERENCE ON CONTROL AND AUTOMATION (ICCA) | 2013年
基金
中国国家自然科学基金;
关键词
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 tracking control for air-breathing hypersonic vehicles in cruising flight is studied, where the super-twisting algorithm is utilized to design a continuous controller. The nonlinear transformation is used to clarify a control-oriented model for hypersonic vehicles. A second order sliding mode controller based on the super-twisting algorithm is designed for the tracking of velocity and altitude, and Lyapunov approach is involved to analyze the stability of closed loop system, which also demonstrates that sliding mode surfaces converge in a finite time. The super-twisting sliding mode control has the ability to reduce chattering and also is robust against varying parameters. Simulations are shown to validate that the proposed method has reduced chattering efficiently and the robustness has been also guaranteed.
引用
收藏
页码:522 / 527
页数:6
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