A control system of a flight vehicle automatically varies the relationship between the center of gravity and the center of pressure of the flight vehicle. The control system automatically adjusts a center of pressure of the flight vehicle depending on a varying payload or payload type that is removably couplable to the flight vehicle. The control system automatically limits translational movement of the one or more wings of the flight vehicle in response to coupling of a payload to a fuselage of the flight vehicle.


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    Titel :

    Flight vehicle wing positioning system


    Beteiligte:
    KOESSLER JEFFREY H (Autor:in) / LEE ANTHONY O (Autor:in) / TRETSCHOK CODY D (Autor:in) / ARTZ GREGORY J (Autor:in)

    Erscheinungsdatum :

    16.06.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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