Contemporary land-survey mini-satellites have general mass up to 500 kg and are placed onto the orbit altitudes up to 800 km. For such spacecraft some principle problems on optimal attitude guidance and robust control are considered and elaborated methods are presented for their solving.


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    Titel :

    Attitude guidance and control of land-survey mini-satellite


    Beteiligte:
    Somov, Yevgeny (Autor:in) / Butyrin, Sergey (Autor:in) / Somov, Sergey (Autor:in) / Salmin, Vadim (Autor:in)


    Erscheinungsdatum :

    01.06.2015


    Format / Umfang :

    930947 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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