H∞ Control for Tracking Targets of Aero-engines

被引：0
|
作者：
Zhu, Fei [1 ]
Sun, Xi-Ming [1 ]
Wu, Yu-Yu [1 ]
机构：
[1] Dalian Univ Technol, Sch Control Sci & Engn, Dalian 116024, Peoples R China
来源：
PROCEEDINGS OF THE 35TH CHINESE CONTROL CONFERENCE 2016 | 2016年
基金：
中国国家自然科学基金;
关键词：
Switched LPV systems; H-infinity tracking control; Aero-engines control; Hysteresis switching; SYSTEMS; STABILITY;
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：
An H-infinity controller design technique for tracking targets is proposed based on a switched model of an aero-engine. Firstly, a switched LPV model is constructed using gain-scheduling parameters, which owns the advantages of nonlinearity and real time observation. Secondly, a sufficient theoretical criterion is provided to guarantee the H-infinity performance in the format of linear matrix inequalities (LMIs), where the switched controllers can be easily constructed by utilizing LMIs Toolbox in Matlab. Finally, simulation results are given to show the validity of the proposed design method.
引用
收藏
页码：5879 / 5884
页数：6
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