Adaptive fault-tolerant flutter control based on dynamic output feedback

被引：1

作者：

Gao, Mingzhou ^{[1
,2
]}

Wang, Qishuai ^{[3
]}

Xu, Dezhi ^{[4
]}

Qu, Yegao ^{[2
]}

Meng, Guang ^{[2
]}

机构：

[1] Jiangnan Univ, Sch Mech Engn, Wuxi 214122, Peoples R China

[2] Shanghai Jiao Tong Univ, State Key Lab Mech Syst & Vibrat, Shanghai 200240, Peoples R China

[3] Shanghai Jiao Tong Univ, Dept Engn Mech, State Key Lab Ocean Engn, Shanghai 200240, Peoples R China

[4] Jiangnan Univ, Sch Internet Things Engn, Wuxi 214122, Peoples R China

来源：

JOURNAL OF THE FRANKLIN INSTITUTE-ENGINEERING AND APPLIED MATHEMATICS | 2023年 / 360卷 / 01期

基金：

中国博士后科学基金; 上海市自然科学基金; 中国国家自然科学基金;

关键词：

SUPERSONIC AIR-FLOW; SUPPRESSION; SYSTEMS; PANEL;

D O I：

10.1016/j.jfranklin.2022.10.003

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

In this paper, the problem of two-dimensional wing flutter control with sensor , actuator failures is studied. Firstly, the aeroelastic equations of motion for two-dimensional wing with plunge and pitch are established; then the wing flutter model with failure modes is established considering the failure modes of sensor and actuator. Secondly, by designing a novel adaptive fault-tolerant controller, the wing flutter can be suppressed effectively and the external disturbance can be dealt with successfully. The stability of the system is proved by the constructed Lyapunov function. Finally, numerical simulation results show that the adaptive flutter fault-tolerant controller can effectively suppress wing flutter when sensors and actuators fail , the controller has good robustness to the changes of external disturbances.(c) 2022 The Franklin Institute. Published by Elsevier Ltd. All rights reserved.

引用

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页码：508 / 526

页数：19

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