To meet requirements of both satellite and Inertial Attitude Sensor(IAS), combination damper is used. First, the fundamental structure of combination damper is presented in this paper. Second, to validate the effect of design, the characteristic of combination damper of 3+1S mode IAS is analyzed by finite element model. Last, the result of experimental verification is provided.


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    Titel :

    Design of combination damper of an inertial attitude sensor


    Beteiligte:
    Li, Sun (Autor:in) / Lu, Liang (Autor:in) / Song, Lin (Autor:in)


    Erscheinungsdatum :

    2014-08-01


    Format / Umfang :

    265187 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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