Robust Fault Tolerant Tracking Control Design for a Linearized Hypersonic Vehicle with Sensor Fault

被引:37
作者
Gao, Zhi-Feng [1 ]
Lin, Jin-Xing [1 ]
Cao, Teng [1 ]
机构
[1] Nanjing Univ Posts & Telecommun, Coll Automat, Nanjing 210046, Jiangsu, Peoples R China
基金
中国国家自然科学基金;
关键词
Fault tolerant control; hypersonic vehicle; sensor fault; tracking control; SWITCHING CONTROL; FLIGHT VEHICLE;
D O I
10.1007/s12555-014-0169-2
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 study, the robust fault tolerant tracking problem is investigated for a linearized hypersonic vehicle model with the bounded external disturbance and the sensor fault. Firstly, the nonlinear longitudinal dynamics of hypersonic vehicle is linearized as a linear time-invariant system with sensor fault, a reference model is introduced for the aim of fault tolerant tracking control. And then an observer-based fault tolerant output feedback tracking controller design approach is proposed by using the linear matrix inequalities (LMIs) technique. The asymptotic stability of the whole closed-loop system is analyzed using the well-known Lyapunov stability method. Finally, the simulation results are presented to verify the applicability of the developed fault tolerant approach.
引用
收藏
页码:672 / 679
页数:8
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