The paper concentrates on the problem of fault-tolerant control of UAV against actuator faults from the perspective of flight control system architecture. Using backstepping control method and inverse optimization theory, the design of backstepping optimal control law was constructed. Based on the fault monitoring mechanism of vehicle management computer in the distributed flight control and control allocation system, a fault-tolerant control design method was established in the case of multiple failure modes of the actuators, which compensates the influence caused by the failures. Finally, the effectiveness of the proposed strategy was verified by numerical simulation.


    Access

    Download


    Export, share and cite



    Title :

    Reconfiguration Control Design of UAV against Actuator Faults Based on Control Allocation Method


    Contributors:
    Yuwei Cui (author) / Aijun Li (author) / Biao Duan (author) / Shabbir Wasif (author)


    Publication date :

    2022




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    Unknown




    Control allocation and re-allocation for a modified quadrotor helicopter against actuator faults

    Sadeghzadeh, Iman / Chamseddine, Abbas / Zhang, Youmin et al. | Tema Archive | 2012


    Control allocation for spacecraft under actuator faults

    Hu, Qinglei / Li, Bo / Xiao, Bing et al. | TIBKAT | 2021


    Reconfiguration control method for non-redundant actuator faults on unmanned aerial vehicle

    Boche, Adèle / Farges, Jean-Loup / De Plinval, Henry | SAGE Publications | 2020


    Reliable Automatic Landing Control Against Actuator Stuck Faults

    Liao, Fang / Wang, Jian / Poh, Eng et al. | AIAA | 2004


    Robust Adaptive Control Allocation for an Octocopter under Actuator Faults

    Yoon, Hyung-Jin / Cichella, Venanzio / Hovakimyan, Naira | AIAA | 2016