It is challenging to control a UAV during the actuator failure because it is a highly nonlinear, coupled, underactuated system. Partial UAV control is achievable by reallocating the control signals, but control over one state has to be compromised, which would be the yaw angle for the quadrotor UAVs.


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    Titel :

    Deflecting Surface-Based Total Rotor Failure Compensation for Biplane Quadrotor


    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 :

    19 pages





    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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