The fixed-Wang, Jie trajectory tracking problem of a quadrotor with six Ma, Xiao of freedom (6-DOF) under bounded disturbances Zhang, Gaowei investigated in this paper. The split-loop design Zhang, Yan which divides the quadrotor into position Miao, Qing and attitude subsystem is adopted. Next, the nonsingular fixed-time controllers are developed and both the inner and outer loop can track the expected trajectory within fixed-time. The settling time depends only on the selected control parameters and is independent of the system’s initial state. The stability of the entire system is proved. Finally, the simulation studies based on the quadrotor model illustrate the robustness of the designed fixed-time controller.


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    Titel :

    Fixed-Time Terminal Sliding Mode Control for Quadrotor Aircraft


    Weitere Titelangaben:

    Lect. Notes Electrical Eng.


    Beteiligte:
    Wang, Rui (Herausgeber:in) / Chen, Zengqiang (Herausgeber:in) / Zhang, Weicun (Herausgeber:in) / Zhu, Quanmin (Herausgeber:in) / Wang, Jie (Autor:in) / Ma, Xiao (Autor:in) / Zhang, Gaowei (Autor:in) / Zhang, Yan (Autor:in) / Miao, Qing (Autor:in)


    Erscheinungsdatum :

    04.12.2019


    Format / Umfang :

    9 pages





    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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