Aiming at the difficulty of precise flight fault-tolerant control of civil aircraft under actuator fault and parameters uncertainties, an intelligent Fault-tolerant control(FTC) method based on Reinforcement Learning-Incremental Nonlinear Dynamic Inversion(RL-INDI) is proposed. The INDI control method is used to solve the model uncertainty caused by actuator fault. The reinforcement learning algorithm is used to interact with the external environment, train and adjust the parameters of the INDI controller according to the system state, and realize the precise flight fault-tolerant control. Finally, the simulation results of the Cessna550 aircraft show that the proposed RL-INDI based intelligence fault-tolerant control method has better performance. The control error is reduced by 9.2, 0.25, 1.3(rad/s) respectively, and the adjustment time is shortened by 0.6, 0.08, 1.04(s) respectively.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Reinforcement Learning-Incremental Nonlinear Dynamic Inversion Based Intelligent Fault-Tolerant Control


    Additional title:

    Lect. Notes Electrical Eng.


    Contributors:
    Yan, Liang (editor) / Duan, Haibin (editor) / Deng, Yimin (editor) / Zhang, Qian (author) / Liu, Shiqian (author) / Lyu, Weizhi (author) / Yang, Congjie (author) / Ruan, Jingzhou Dai (author) / Chen, Han (author)

    Conference:

    International Conference on Guidance, Navigation and Control ; 2024 ; Changsha, China August 09, 2024 - August 11, 2024



    Publication date :

    2025-02-27


    Size :

    11 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


    Fault-Tolerant Control of Wing Surface Based on Incremental Nonlinear Dynamic Inversion

    Chen, Jiaxin / Liu, Xiaoxiong / Chen, Tongwen et al. | Springer Verlag | 2025


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

    Cheng, Huihui / Liu, Shiqian / Ma, Xinjian et al. | Springer Verlag | 2021