Gain-scheduled control for morphing aircraft via switching polytopic linear parameter-varying systems

被引：33

作者：

Jiang, Weilai ^{[1
]}

Wu, Kangsheng ^{[1
]}

Wang, Zhaolei ^{[2
]}

Wang, Yaonan ^{[1
]}

机构：

[1] Hunan Univ, Coll Elect & Informat Engn, Changsha 410082, Peoples R China

[2] Beijing Aerosp Automat Control Inst, Beijing 100854, Peoples R China

来源：

AEROSPACE SCIENCE AND TECHNOLOGY | 2020年 / 107卷

基金：

中国国家自然科学基金;

关键词：

Morphing aircraft; Switching polytopic linear; parameter-varying systems; Multiple parameter-dependent Lyapunov functions; Average dwell time; Mode-dependent average dwell time;

D O I：

10.1016/j.ast.2020.106242

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

This paper addresses the gain-scheduled output feedback control for morphing aircraft (MA) in full envelope using switching polytopic linear parameter-varying (SPLPV) theory. The SPLPV model of MA is derived by scheduled parameter interval division and convex decomposition. Considering average dwell time (ADT) and mode-dependent average dwell time (MDADT) switching logics, sufficient conditions to ensure that the SPLPV systems are exponential stable with weighted disturbance attenuation indexes are presented based on the multiple parameter-dependent Lyapunov functions (MPDLFs) technique, and the comprehensive algorithm for the controller solution is obtained. To reduce the computational burden and ease controller implementation, a finite number of linear matrix inequalities (LMIs) are developed for solving controller by proposing the intermediate controller variables are depend affinely on the scheduled parameter. In addition, the control matrix of linear parameter-varying (LPV) system is not limited to be constant, which greatly expands the application scope of the proposed method. The simulation validation is carried out on the SPLPV control for MA. (c) 2020 Elsevier Masson SAS. All rights reserved.

引用

页数：16

共 33 条

[1] Morphing aircraft: The need for a new design philosophy [J].

Ajaj, Rafic M. ;

Beaverstock, Christopher S. ;

Friswell, Michael I. .

AEROSPACE SCIENCE AND TECHNOLOGY, 2016, 49 :154-166

[2]

Apkarian P, 2000, ADV DES CONTROL, P209, DOI 10.1137/1.9780898719833.ch11

[3] SELF-SCHEDULED H-INFINITY CONTROL OF LINEAR PARAMETER-VARYING SYSTEMS - A DESIGN EXAMPLE [J].

APKARIAN, P ;

GAHINET, P ;

BECKER, G .

AUTOMATICA, 1995, 31 (09) :1251-1261

[4] Modeling and Control of an Aeroelastic Morphing Vehicle [J].

Baldelli, Dario H. ;

Lee, Dong-Hwan ;

Sanchez Pena, Ricardo S. ;

Cannon, Bryan .

JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2008, 31 (06) :1687-1699

[5]

BECKER G, 1993, PROCEEDINGS OF THE 1993 AMERICAN CONTROL CONFERENCE, VOLS 1-3, P2795

[6] Non-fragile switched H∞ control for morphing aircraft with asynchronous switching [J].

Cheng, Haoyu ;

Dong, Chaoyang ;

Jiang, Weilai ;

Wang, Qing ;

Hou, Yanze .

CHINESE JOURNAL OF AERONAUTICS, 2017, 30 (03) :1127-1139

[7] H infinity design with pole placement constraints: An LMI approach [J].

Chilali, M ;

Gahinet, P .

IEEE TRANSACTIONS ON AUTOMATIC CONTROL, 1996, 41 (03) :358-367

[8] Gain-scheduled H∞ control via parameter-dependent Lyapunov functions [J].

Chumalee, Sunan ;

Whidborne, James F. .

INTERNATIONAL JOURNAL OF SYSTEMS SCIENCE, 2015, 46 (01) :125-138

[9] A LINEAR MATRIX INEQUALITY APPROACH TO H-INFINITY CONTROL [J].

GAHINET, P ;

APKARIAN, P .

INTERNATIONAL JOURNAL OF ROBUST AND NONLINEAR CONTROL, 1994, 4 (04) :421-448

[10] Smooth-switching LPV control for vibration suppression of a flexible airplane wing [J].

He, Tianyi ;

Zhu, Guoming G. ;

Swei, Sean S. -M. ;

Su, Weihua .

AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 84 :895-903

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