Reduced-order H∞ Controller Design Using the μ-synthesis Applied to Lateral Control of Highly Flexible Aircraft

被引：0
|
作者：
Zhang, Li [1 ]
Tang, Shuai [1 ]
Zheng, Zhiqiang [1 ]
机构：
[1] Natl Univ Def Technol, Coll Mechatron & Automat, Changsha 410073, Hunan, Peoples R China
来源：
MECHATRONICS, ROBOTICS AND AUTOMATION, PTS 1-3 | 2013年 / 373-375卷
关键词：
Flexible aircraft dynamics; Model reduction; Balanced-truncation; mu-analysis and synthesis; H-infinity control;
D O I：
10.4028/www.scientific.net/AMM.373-375.1374
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
A lateral flight reduced-order controller for a flexible aircraft is presented. It is based on the reduced-order model of the flexible aircraft and the mu-analysis and synthesis toolbox. The first step deals with the order reduction of the full-model by using the balanced-truncation model reduction method. Then the reduced-order H-infinity. controller is achieved by using the mu-analysis and synthesis theory and applied to the reduced-order model and full-order model of the flexible aircraft. Finally, numerical results are presented and discussed. The simulation results show the efficiency of the reduced-order controller based on the reduced-order model since the close-loop system of the full-order model meets a set of realistic specifications in the frequency and time domains.
引用
收藏
页码：1374 / 1377
页数：4
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