Energy efficient satellite maneuvering is described herein. One disclosed example method includes maneuvering a satellite that is in an orbit around a space body so that a principle sensitive axis of the satellite is oriented to an orbit frame plane to reduce gravity gradient torques acting upon the satellite. The orbit frame plane is based on an orbit frame vector.


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    Title :

    ENERGY EFFICIENT SATELLITE MANEUVERING


    Additional title:

    ENERGIEEFFIZIENTE SATELLITENMANÖVRIERUNG
    MANOEUVRE DE SATELLITE EFFICACE EN ÉNERGIE


    Contributors:
    LUI TIMOTHY S (author) / LEE KANGSIK (author)

    Publication date :

    2019-11-27


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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