Observer-based H-infinity Tracking Control Design for A Linearized Hypersonic Vehicle Model with External Disturbance

被引:0
|
作者
Gao, Zhifeng [1 ]
Cao, Teng [1 ]
Lin, Jinxing [1 ]
Qian, Moshu [2 ]
机构
[1] Nanjing Univ Posts & Telecommun, Coll Automat, Nanjing 210046, Jiangsu, Peoples R China
[2] Nanjing Univ Aeronaut & Astronaut, Res Inst UAV, Nanjing 210016, Jiangsu, Peoples R China
来源
2014 IEEE CHINESE GUIDANCE, NAVIGATION AND CONTROL CONFERENCE (CGNCC) | 2014年
关键词
SWITCHING CONTROL; FLIGHT VEHICLE;
D O I
暂无
中图分类号
TM [电工技术]; TN [电子技术、通信技术];
学科分类号
0808 ; 0809 ;
摘要
In this study, the H-infinity tracking control problem of a linearized hypersonic vehicle model with the bounded external disturbance is investigated. Firstly, the nonlinear longitudinal dynamics of hypersonic vehicle is linearized as a linear time-invariant system with the bounded external disturbance, a reference model is introduced for the aim of tracking control. And then an observer-based output feedback tracking controller design approach is proposed by using the linear matrix inequalities (LMIs) technique. The asymptotical stability of the closed-loop system is analyzed in the framework of Lyapunov method. Finally, the simulation results are given to illustrate the applicability of the developed control approach.
引用
收藏
页码:1649 / 1653
页数:5
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