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.

    Il est décrit des manuvres de satellite à haut rendement énergétique. Un exemple décrit comprend manuvrer un satellite orbitant un astre de sorte quun axe sensible principal du satellite soit orienté vers un plan de cadre dorbite en vue de réduire les couples de gradient de gravité qui agissent sur le satellite. Le plan du cadre dorbite est basé sur un vecteur du cadre dorbite.


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    Title :

    ENERGY EFFICIENT SATELLITE MANEUVERING


    Additional title:

    MANOEUVRE DE SATELLITE A EFFICACITE ENERGETIQUE


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

    Publication date :

    2022-02-15


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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