An unmanned aerial vehicle including a body, a platform, a rotor, a tether cable, and an actuation system. The platform is coupled to the body such that the platform is rotatable relative to the body about a first horizontal axis of rotation. The rotor is rigidly coupled to the platform such that the rotor and the platform rotate together about the first horizontal axis of rotation. The tether cable extends away from the body and is coupled to the body such that the tether cable is rotatable relative to the body about a second horizontal axis of rotation. The first and second horizontal axes of rotation are normal to a vertical plane. The actuation system is configured to rotate the platform in a clockwise direction about the first horizontal axis of rotation when the tether cable rotates in a counter-clockwise direction about the second horizontal axis of rotation.


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    Titel :

    STABILITY SYSTEMS FOR TETHERED UNMANNED AERIAL VEHICLES


    Beteiligte:
    BUYSE MATHIEU (Autor:in) / COULON JEAN MARC (Autor:in) / BLAVIER MIKE (Autor:in)

    Erscheinungsdatum :

    2021-01-21


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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