This paper established a damaged aircraft model and developed a fault-tolerant controller based on incremental nonlinear dynamic inversion with prescribed performance to enhance flight safety. This fault-tolerant controller can rapidly stabilize the damaged aircraft, and tracking error is always within the prescribed boundaries in the whole process. Thus, the transient and steady-state performance of the damaged aircraft is guaranteed. Simulation results demonstrate that the developed fault-tolerant controller can achieve satisfactory control performance and improve aircraft flight safety.


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    Titel :

    An Incremental Nonlinear Dynamic Inversion with Prescribed Performance for Damaged Aircraft


    Weitere Titelangaben:

    Lect. Notes Electrical Eng.


    Beteiligte:
    Yan, Liang (Herausgeber:in) / Duan, Haibin (Herausgeber:in) / Deng, Yimin (Herausgeber:in) / Li, Yu (Autor:in) / Liu, Xiaoxiong (Autor:in) / Zuo, Qun (Autor:in) / Huang, Wei (Autor:in) / Ming, Ruichen (Autor:in) / Zhang, Weiguo (Autor:in)

    Kongress:

    International Conference on Guidance, Navigation and Control ; 2022 ; Harbin, China August 05, 2022 - August 07, 2022



    Erscheinungsdatum :

    2023-01-31


    Format / Umfang :

    9 pages





    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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