This article presents a non-initial value fault-tolerant prescribed performance control (FTPPC) method for small fixed-wing unmanned aerial vehicles (UAVs) experiencing actuator faults. A novel global finite-time performance function (GFPF) is developed to remove the initial condition limitations inherent in the system. Meanwhile, the output error is ensured to remain within a small vicinity around the equilibrium point in a finite time. The effectiveness is demonstrated by simulations.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Non-initial Value Fault-Tolerant Prescribed Performance Control for Small Fixed-Wing UAVs with Actuator Faults


    Additional title:

    Lect. Notes Electrical Eng.


    Contributors:
    Yan, Liang (editor) / Duan, Haibin (editor) / Deng, Yimin (editor) / Huang, Bo (author) / Wu, Zhonghua (author)

    Conference:

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



    Publication date :

    2025-03-02


    Size :

    9 pages





    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English