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

页码：1374 / 1377

页数：4

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