Fault Tolerant Control Based on Thau Observer of a Reconfigurable Quadrotor with Total Loss of Actuator

被引:5
|
作者
Salmi, Abdenour [1 ]
Guiatni, Mohamed [1 ]
Bouzid, Yasser [1 ]
Derrouaoui, Saddam Hocine [1 ]
Boudjema, Fares [2 ]
机构
[1] Ecole Mil Polytech, Complex Syst Control & Simulators Lab, Algiers, Algeria
[2] Ecole Natl Polytech, Proc Control Lab, Algiers, Algeria
关键词
Reconfigurable quadrotor; trajectory tracking; active FTC; nonlinear Thau observer; sliding mode control; foldable arms; rotor total loss of effectiveness; control allocation; SLIDING MODE CONTROL; DESIGN; DRONE;
D O I
10.1142/S2301385024500146
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, we propose a Fault Tolerant Control (FTC) strategy for a reconfigurable quadrotor with foldable arms, to deal with a total loss of one of its rotors. The proposed strategy allows adapting the configuration of the quadrotor when one of its rotors is lost. It consists of: (i) a Fault Detection and Isolation (FDI) module, (ii) a robust controller, and (iii) a reconfiguration module. The FDI module is designed based on the nonlinear Thau observer in order to detect and identify the rotors faults. Once a rotor fault is detected based on the residual analysis, the quadrotor changes its shape by rotating the two adjacent arms in the direction of damaged one in order to form a trirotor configuration. This transformation induces a variation of vehicle's center of gravity (CoG), inertia, and consequently the control matrix. To deal with this issue, a sliding mode controller (SMC) is designed based on the control allocation matrix, where the control efforts are redistributed among healthy actuators. Numerical simulations are carried out to verify the effectiveness of the proposed approach. The obtained results show that the proposed strategy is successful in controlling the damaged quadrotor by trajectory tracking.
引用
收藏
页码:667 / 683
页数:17
相关论文
共 50 条
  • [1] SYSTEMATIC FAULT TOLERANT CONTROL BASED ON ADAPTIVE THAU OBSERVER ESTIMATION FOR QUADROTOR UAVs
    Cen, Zhaohui
    Noura, Hassan
    Al Younes, Younes
    [J]. INTERNATIONAL JOURNAL OF APPLIED MATHEMATICS AND COMPUTER SCIENCE, 2015, 25 (01) : 159 - 174
  • [2] Fault Tolerant Control of Actuator Additive Fault for Quadrotor Based on Sliding Mode Observer
    Zheng, Jiajing
    Li, Ping
    [J]. PROCEEDINGS OF THE 2019 31ST CHINESE CONTROL AND DECISION CONFERENCE (CCDC 2019), 2019, : 5908 - 5913
  • [3] Observer based finite-time fault tolerant quadrotor attitude control with actuator faults
    Tang, Pan
    Lin, Defu
    Zheng, Duo
    Fan, Shipeng
    Ye, Jianchuan
    [J]. AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 104
  • [4] Disturbance Observer Based Fault Tolerant Control of a Quadrotor Helicopter
    Hocaoglu, Yarkin
    Mumcuoglu, Mehmet Emin
    Unel, Mustafa
    [J]. IECON 2021 - 47TH ANNUAL CONFERENCE OF THE IEEE INDUSTRIAL ELECTRONICS SOCIETY, 2021,
  • [5] Actuator fault tolerant control based on neuroadaptive SMC for Quadrotor UAVs
    Liu, Fei
    Hou, Xiaojian
    Wang, Renjie
    Yu, Yao
    [J]. 2020 35TH YOUTH ACADEMIC ANNUAL CONFERENCE OF CHINESE ASSOCIATION OF AUTOMATION (YAC), 2020, : 144 - 149
  • [6] A Fault Tolerant Control Design for Actuator Fault Mitigation in Quadrotor UAVs
    Mallavalli, Seema
    Fekih, Afef
    [J]. 2019 AMERICAN CONTROL CONFERENCE (ACC), 2019, : 5111 - 5116
  • [7] ACTUATOR FAULT TOLERANT CONTROL DESIGN BASED ON A RECONFIGURABLE REFERENCE INPUT
    Theilliol, Didier
    Join, Cedric
    Zhang, Youmin
    [J]. INTERNATIONAL JOURNAL OF APPLIED MATHEMATICS AND COMPUTER SCIENCE, 2008, 18 (04) : 553 - 559
  • [8] Actuator Fault Tolerant Control of Variable Pitch Quadrotor Vehicles
    Baldini, Alessandro
    Felicetti, Riccardo
    Freddi, Alessandro
    Longhi, Sauro
    Monteriu, Andrea
    [J]. IFAC PAPERSONLINE, 2020, 53 (02): : 4095 - 4102
  • [9] Adaptive Fault Tolerant Control for a Quadrotor Under Actuator Faults
    Wang, Xian
    Zhao, Jing
    Qian, Juan
    Xie, Fei
    Fu, Jiang
    [J]. PROCEEDINGS OF THE 38TH CHINESE CONTROL CONFERENCE (CCC), 2019, : 5079 - 5084
  • [10] Fault-tolerant control of hypersonic vehicles based on fast fault observer under actuator gain loss fault or stuck fault
    Zhu, P.
    Jiang, J.
    Yu, C.
    [J]. AERONAUTICAL JOURNAL, 2020, 124 (1278): : 1190 - 1207