We present method for in-flight signal processing and calibration of a strap-down inertial navigation system (SINS) for the information mini-satellites at low Earth orbit. We have applied the SINS correction based on the signals of a sun-magnetic system and consider the problem at a long-term forecasting of the mini-satellite's orbital motion.


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    Titel :

    Low cost attitude determination system for a LEO information mini-satellite


    Beteiligte:
    Somov, Yevgeny (Autor:in) / Butyrin, Sergey (Autor:in) / Somov, Sergey (Autor:in) / Hajiyev, Chingiz (Autor:in)


    Erscheinungsdatum :

    01.06.2015


    Format / Umfang :

    1349166 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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