Robust and fault tolerant controller for attitude control of a satellite launch vehicle

被引：34
|
作者：
Das, R. K. [1 ]
Sen, S.
Dasgupta, S.
机构：
[1] Indian Inst Technol, Dept Elect Engn, Kharagpur 721302, W Bengal, India
[2] Noorul Islam Coll Engn, Dept Elect & Elect Engn, Kumarcoil, Tamil Nadu, India
来源：
IET CONTROL THEORY AND APPLICATIONS | 2007年 / 1卷 / 01期
关键词：
D O I：
10.1049/iet-cta:20050518
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
The design of a robust and fault-tolerant control system for the attitude control of a satellite launch vehicle is described. The robust controller is designed for the nominal system in order to reduce the effect of disturbances in the system. Finally, a reconfigured controller is designed to stabilise the system by placing the closed-loop poles within a desired region and also to guarantee the disturbance attenuation below a certain level. The linear matrix inequality technique is used to design the controllers. The performance of the nominal and reconfigured controller is presented.
引用
收藏
页码：304 / 312
页数：9
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