The invention relates to a method (100) for controlling the orbit of a satellite, which method comprises: - determining (102) a manoeuvre plan (PMA) comprising at least one previous manoeuvre (PM1) of the previous manoeuvre plan (PPMA), if the at least one previous manoeuvre (PM1 = MA1) is implemented on a date corresponding to a previous fixed part (PPF) and the prediction horizon (HP), the manoeuvre plan (PMA) comprising at least one manoeuvre (MA2, MA3) implemented during a part of the prediction horizon; - identifying (103) a collision risk; - determining (104) a new manoeuvre plan (NPMA) comprising a previous manoeuvre (PM1, PM2, PM3) of the previous manoeuvre plan (PPMA), if the previous manoeuvre is implemented within the previous prediction horizon (PHP) and the prediction horizon (HP) of the new manoeuvre plan (NPMA), and comprising a new manoeuvre (NMA4), implemented over a new part of the prediction horizon (HP).


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    Title :

    PROCÉDÉ POUR UN CONTRÔLE D'ORBITE AUTONOME ET SATELLITE CONFIGURÉ POUR LA MISE EN OEUVRE DU PROCÉDÉ


    Additional title:

    METHOD FOR AUTONOMOUS ORBIT CONTROL AND SATELLITE CONFIGURED TO IMPLEMENT THE METHOD
    VERFAHREN ZUR AUTONOMEN ORBIT-STEUERUNG UND SATELLIT MIT KONFIGURATION ZUR IMPLEMENTIERUNG DES VERFAHRENS


    Contributors:

    Publication date :

    2025-02-05


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS