Sliding mode output feedback controller design using linear matrix inequalities with application to aircraft systems

被引：1
|
作者：
Andrade-Da Silva, Jose Manuel [1 ]
Spurgeon, Sarah K. [1 ]
Edwards, Christopher [1 ]
机构：
[1] Univ Leicester, Dept Engn, Control & Instrumentat Res Grp, Leicester LE1 7RH, Leics, England
来源：
2008 INTERNATIONAL WORKSHOP ON VARIABLE STRUCTURE SYSTEMS | 2008年
关键词：
D O I：
10.1109/VSS.2008.4570712
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 problem of designing a sliding mode controller for uncertain MIMO dynamical systems with matched and unmatched uncertainties using only measured output signals is addressed. A design methodology based on LMI's under a polytopic formulation is presented for the existence and reachability problems. The proposed controller is static in nature. The reaching and sliding motion are guaranteed despite the presence of both matched and unmatched uncertainties. A design study involving the lateral control of an aircraft is employed in order to illustrate the efficacy of the approach developed.
引用
收藏
页码：227 / 232
页数：6
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