A structure for changing the attitude of a spacecraft is provided including an elongated member and a plurality of actuators coupled to the elongated member. The elongated member is coupled to the spacecraft. The elongated member has a length and an angular position relative to an axis. The plurality of actuators are configured to deflect the angular position of the elongated member relative to the axis and to alter the length of the elongated member.


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    Title :

    MULTIFUNCTIONAL STRUCTURES FOR ATTITUDE CONTROL


    Additional title:

    MULTIFUNKTIONSSTRUKTUREN ZUR LAGEREGELUNG
    STRUCTURES MULTIFONCTIONNELLES POUR LA COMMANDE D'ATTITUDE


    Contributors:
    VEDANT (author) / ALLISON JAMES T (author)

    Publication date :

    2023-06-21


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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