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 | 2023年 / 360卷 / 01期
基金：
中国国家自然科学基金; 上海市自然科学基金; 中国博士后科学基金;
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
收藏
页码：508 / 526
页数：19
相关论文
共 25 条
  • [1] Active control of nonlinear panel flutter under yawed supersonic flow
    Abdel-Motagaly, K
    Guo, XY
    Duan, B
    Mei, C
    [J]. AIAA JOURNAL, 2005, 43 (03) : 671 - 680
  • [2] Active flutter control of thin walled wing-engine system using piezoelectric actuators
    Asadi, Davood
    Farsadi, Touraj
    [J]. AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 102
  • [3] Bertin J.J., 1994, HYPERSONIC AEROTHERM
  • [4] Equivalent damping of aeroelastic system of an airfoil with cubic stiffness
    Chen, Y. M.
    Liu, J. K.
    Meng, G.
    [J]. JOURNAL OF FLUIDS AND STRUCTURES, 2011, 27 (08) : 1447 - 1454
  • [5] Cheng P., 2021, IEEE T CYBERN
  • [6] Learning-Based Distributed Resilient Fault-Tolerant Control Method for Heterogeneous MASs Under Unknown Leader Dynamic
    Deng, Chao
    Jin, Xiao-Zheng
    Che, Wei-Wei
    Wang, Hai
    [J]. IEEE TRANSACTIONS ON NEURAL NETWORKS AND LEARNING SYSTEMS, 2022, 33 (10) : 5504 - 5513
  • [7] Adaptive optimization algorithm for nonlinear Markov jump systems with partial unknown dynamics
    Fang, Haiyang
    Zhu, Guozheng
    Stojanovic, Vladimir
    Nie, Rong
    He, Shuping
    Luan, Xiaoli
    Liu, Fei
    [J]. INTERNATIONAL JOURNAL OF ROBUST AND NONLINEAR CONTROL, 2021, 31 (06) : 2126 - 2140
  • [8] Analysis and synthesis of robust control systems using linear parameter dependent Lyapunov functions
    Geromel, Jose C.
    Korogui, Rubens H.
    [J]. IEEE TRANSACTIONS ON AUTOMATIC CONTROL, 2006, 51 (12) : 1984 - 1989
  • [9] Aeroelastic analysis and active flutter suppression of an electro-rheological sandwich cylindrical panel under yawed supersonic flow
    Hasheminejad, Seyyed M.
    Motaaleghi, M. Aghayi
    [J]. AEROSPACE SCIENCE AND TECHNOLOGY, 2015, 42 : 118 - 127
  • [10] Improved bounded-real-lemma representation and H∞ control of systems with polytopic uncertainties
    He, Y
    Wu, M
    She, JH
    [J]. IEEE TRANSACTIONS ON CIRCUITS AND SYSTEMS II-EXPRESS BRIEFS, 2005, 52 (07) : 380 - 383
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