The invention relates to an angular momentum unloading method of a small-sized momentum wheel. The angular momentum unloading of the small-sized momentum wheel is carried out by adopting a magnetic torque on a satellite when the angular momentum is not saturated in the normal control period of the small-sized momentum wheel; when the angular momentum of the small-sized momentum wheel is saturated, the surplus angular momentum of the small-sized momentum wheel is unloaded in priority by utilizing a satellite platform momentum wheel; if the satellite platform momentum wheel is also saturated, the angular momentum is unloaded by utilizing an injection way by virtue of a thrustor on the satellite.


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    Titel :

    Angular momentum unloading method of small-sized momentum wheel


    Beteiligte:
    LI MINGQUN (Autor:in) / WANG SHUYI (Autor:in) / GONG YULIAN (Autor:in) / CHU YONGHUI (Autor:in) / XING LINFENG (Autor:in) / HAO JINHUA (Autor:in) / DONG YUN (Autor:in) / LI HE (Autor:in) / DU HUI (Autor:in) / XU ZILI (Autor:in)

    Erscheinungsdatum :

    12.08.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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