One of the core ideas behind the development of UAVs is payload delivery in remote areas. For such applications, a biplane quadrotor is a better choice than the rotary-wing UAVs because after the payload delivery biplane quadrotor can fly like a fixed-wing UAV and get back to the origin, which saves energy and time. This chapter proposes a novel control structure to stabilize a slung load attached to the vehicle.


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    Titel :

    Anti-Swing Control Structure for the Biplane Quadrotor with Slung Load


    Weitere Titelangaben:

    Studies in Systems, Decision and Control


    Beteiligte:
    Dalwadi, Nihal (Autor:in) / Deb, Dipankar (Autor:in) / Ozana, Stepan (Autor:in)


    Erscheinungsdatum :

    24.02.2023


    Format / Umfang :

    21 pages





    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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