Various reconfigurations of wing sections of a ring wing of an aerial vehicle are described. For example, responsive to a fault or failure of a propulsion mechanism, one or more wing sections may be modified to maintain control and safety of the aerial vehicle. In example embodiments, positions, angular orientations, and/or pitches of one or more wing sections may be modified to maintain control and safety in either a horizontal, wingborn flight orientation, or a vertical, VTOL flight orientation.


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    Titel :

    Six degree of freedom aerial vehicle having reconfigurable wings


    Beteiligte:
    LEGRAND LOUIS (Autor:in) / RAND OMRI (Autor:in) / KIMCHI GUR (Autor:in) / FISCHER SEBASTIAN (Autor:in) / WELSH RICKY (Autor:in)

    Erscheinungsdatum :

    2021-04-20


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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