The invention discloses a pentagonal pyramid control moment gyro group vibration isolation support integrated device which comprises an upper platform, a middle platform arranged below the upper platform, a lower platform arranged below the middle platform and a plurality of vibration isolator branch supporting legs. Gyro groups are arranged between the upper platform and the middle platform. The vibration isolator branch supporting legs are arranged between the middle platform and the lower platform. A vibration isolator and a pentagonal pyramid control moment gyro group support are integrally designed, so that mounting errors caused in the system assembling process are reduced, high-precision moment output of the control moment gyro groups is guaranteed, and the maneuvering and attitude holding energy of an satellite is maintained.


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    Titel :

    Pentagonal pyramid control moment gyro group vibration isolation support integrated device


    Beteiligte:
    SUN HONGLI (Autor:in) / LI JIEDONG (Autor:in) / TAN TIANLE (Autor:in) / HE LIANG (Autor:in) / ZHU QINGHUA (Autor:in) / ZHU DONGFANG (Autor:in) / YANG GUANG (Autor:in)

    Erscheinungsdatum :

    28.10.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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