Aircraft Engine decentralized tracking control: a new LMI Approach

被引：0

作者：

Cao, Liangjin ^{[1
]}

Pan, Muxuan ^{[1
]}

机构：

[1] Nanjing Univ Aeronaut & Astronaut, Fac Jiangsu Prov Key Lab Aerosp Power Syst, Nanjing 210016, Jiangsu, Peoples R China

来源：

2017 9TH INTERNATIONAL CONFERENCE ON MODELLING, IDENTIFICATION AND CONTROL (ICMIC 2017) | 2017年

基金：

中国国家自然科学基金;

关键词：

Decentralized tracking control; linear matrix inequalities method; Aircraft Engine; OUTPUT-FEEDBACK CONTROL; LARGE-SCALE SYSTEMS; CONTROL DESIGN; ROBUST-CONTROL;

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 decentralized tracking control of large-scale systems. The novelty of the paper comes from the consideration of introducing adjustable parameters to linear matrix inequalities (LMI). These adjustable parameters can adjust the convergent rate of tracking error signals and the coupling between subsystems. This method is applied to aircraft engine decentralized tracking control, simulation results have shown its validity.

引用

下载

页码：764 / 769

页数：6

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