A reaction wheel detects an angular momentum. A satellite controller selects a target thruster based on the detected angular momentum. A power supply apparatus changes adjustment electric power for the target thruster. A flow rate adjustment apparatus supplies a propellant to the target thruster at a flow rate corresponding to the adjustment electric power. This changes a thrust of the target thruster. When a discharge current of the target thruster does not become a target current, the power supply apparatus further changes the adjustment electric power for the target thruster.


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    Titel :

    ARTIFICIAL SATELLITE AND THRUST BALANCE ADJUSTMENT METHOD


    Beteiligte:
    HOSODA MASAYA (Autor:in) / TANAKA YUTARO (Autor:in) / NAKAGAWA TAKAFUMI (Autor:in)

    Erscheinungsdatum :

    16.05.2019


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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