In this paper, a control scheme is developed for attitude system of a fixed-wing unmanned aerial vehicle (UAV) subject to unknown external disturbance. First, the dynamic equations of attitude system are introduced and the control-oriented model (COM) is established. Then, an adaptive-gain sliding mode (AGSM) algorithm is proposed to handle the effects of unknown external disturbance such that the expected equivalent sliding-mode dynamics can be obtained. Based on the above design, an actor-critic structure-based ADP approach is employed to generate the nearly optimal control law. Finally, the validity of our proposed control scheme is demonstrated via simulation.


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    Titel :

    Sliding Mode Control for a Fixed-Wing UAV with Disturbance via Adaptive Dynamic Programming


    Weitere Titelangaben:

    Lect.Notes Mechanical Engineering


    Beteiligte:
    Zhang, Chaofan (Autor:in) / Xing, Chenguang (Autor:in) / Liu, Bo (Autor:in) / Du, Ziliang (Autor:in)

    Kongress:

    China Aeronautical Science and Technology Conference ; 2023 ; Wuzhen, China September 26, 2023 - September 27, 2023



    Erscheinungsdatum :

    19.12.2023


    Format / Umfang :

    10 pages





    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch





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