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

来源：

PROCEEDINGS OF THE 2012 24TH CHINESE CONTROL AND DECISION CONFERENCE (CCDC) | 2012年

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

页码：4233 / 4236

页数：4

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