A method (50) for orbit control of a satellite (10) in Earth orbit and for desaturation of an angular momentum storage device of the satellite, the satellite (10) including an articulated arm (21) suitable for moving a propulsion unit (31) within a motion volume included in a half-space delimited by an orbital plane when the satellite is in a mission attitude, the method (50) including a single-arm control mode using only the propulsion unit (31) carried by the articulated arm (21), the single-arm control mode using a maneuvering plan including only thrust maneuvers to be executed when the satellite (10) is located within an angular range of at most 180° centered on a target node in the orbit of the satellite (10), including two thrust maneuvers to be performed respectively upstream and downstream of the target node.


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    Title :

    PROCÉDÉ DE CONTRÔLE D'ORBITE ET DE DÉSATURATION D'UN SATELLITE AU MOYEN D'UN UNIQUE BRAS ARTICULÉ PORTANT UNE UNITÉ DE PROPULSION


    Additional title:

    METHOD FOR ORBIT CONTROL AND DESATURATION OF A SATELLITE BY MEANS OF A SINGLE ARTICULATED ARM CARRYING A PROPULSION UNIT
    VERFAHREN ZUR UMLAUFBAHNSTEUERUNG UND -DESATURATION EINES SATELLITEN MITTELS EINZELGELENKARM, DER EINE ANTRIEBSEINHEIT TRÄGT


    Contributors:

    Publication date :

    2022-10-19


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS