Provided is a satellite orbit controlling method and apparatus. A satellite orbit adjusting method performed at a current satellite may include measuring a distance between the current satellite and another satellite using a radio frequency; calculating a relative location relationship between the current satellite and the other satellite based on the measured distance, and estimating an orbit element based on the location relationship; calculating speed increment information for controlling a maneuver based on the estimated orbit element; and adjusting a satellite orbit of the current satellite based on the speed increment information.


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    Titel :

    METHOD AND APPARATUS FOR CONTROLLING ORBIT OF COLLOCATED SATELLITE


    Beteiligte:
    HWANG YOOLA (Autor:in) / LEE BYOUNG-SUN (Autor:in)

    Erscheinungsdatum :

    07.06.2018


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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