Static Output Feedback For Aeroengine Control System

被引:0
|
作者
Hao, Binbin [1 ]
Qu, Tao [1 ]
机构
[1] AVIC Shenyang Engine Design & Res Inst, Shenyang 110015, Peoples R China
关键词
SISO control; multivariable control; linear matrix inequalities; robust H-2 control; static output feedback; aeroengine; ROBUST STABILITY; LMI CONDITION; TIME;
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
This paper considers the static output feedback control synthesis problem of aeroengine system. By introducing a slack variable for separating system matrix and Lyapunov matrix, more relaxed sufficient conditions for designing static output feedback controller are given in terms of solutions to a set of linear matrix inequalities. Simulation illustrates that the proposed methods for aeroengine systems can achieve good performance.
引用
收藏
页码:4233 / 4236
页数:4
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