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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    Title :

    Attitude guidance and control of land-survey mini-satellite


    Contributors:


    Publication date :

    2015-06-01


    Size :

    930947 byte




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



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