A first inclination vector associated with a first satellite (12) of the plurality of satellites is established. A second inclination vector associated with a second satellite (42) of the plurality of satellites is established. The first satellite and the second satellite are controlled, such that the first satellite and the second satellite are synchronized with a node.


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    Title :

    Methods and apparatus for controlling a plurality of satellites using node-synchronous eccentricity control


    Additional title:

    Verfahren und Vorrichtung zur Steuerung einer Vielzahl von Satelliten mit knotensynchroner Exzentrizitätssteuerung
    Procédés et appareil pour commander une pluralité de satellites au moyen de contrôle d'excentricité de noeuds synchrones


    Contributors:

    Publication date :

    2019-03-20


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS





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