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).


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

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


    Weitere Titelangaben:

    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


    Beteiligte:

    Erscheinungsdatum :

    05.02.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Französisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS