Pilot mishandling and actuator faults are two major factors for safe flight of the civil aircraft. To solve this problem, a fault-tolerant control (FTC) method based on incremental nonlinear dynamic inversion (INDI) is proposed. Firstly, a Hess pilot model and attitude dynamics model are established to describe pilot manipulation and aircraft attitude motions. Based on this model, an INDI control is introduced to realize the aircraft fault tolerant control. The closed-loop system is asymptotically stable. Simulation results show that INDI controllers have better tracking performances than those of NDI controllers, even in the presence of actuator failure and pilot mishandling.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Incremental Nonlinear Dynamic Inversion Based Fault Tolerant Control for Pilot Error and Actuator Faults


    Additional title:

    Lect. Notes Electrical Eng.


    Contributors:
    Yan, Liang (editor) / Duan, Haibin (editor) / Yu, Xiang (editor) / Cheng, Huihui (author) / Liu, Shiqian (author) / Ma, Xinjian (author) / Xie, Xinhong (author)


    Publication date :

    2021-10-30


    Size :

    12 pages





    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English




    Incremental Nonlinear Dynamic Inversion-based Fault-Tolerant Guidance for UAV

    Kim, Yeji / Kim, Seungkeun / Suk, Jinyoung | AIAA | 2024


    Nonlinear robust fault-tolerant control for turbofan engines with actuator faults

    Cheng, Dingding / Liu, Lijun / Yu, Zhen | SAGE Publications | 2023


    Nonlinear Dynamic Inversion with Actuator Dynamics: An Incremental Control Perspective

    Steffensen, Rasmus / Steinert, Agnes / Smeur, Ewoud J. J. | AIAA | 2022



    Fault-Tolerant Adaptive Neural Control of Multi-UAVs Against Actuator Faults

    Yu, Ziquan / Zhang, Youmin / Qu, Yaohong et al. | IEEE | 2019