We consider problems on attitude guidance, navigation and robust gyromoment control of the agile spacecraft for surveying the Earth surface. We present developed methods for dynamic research of the spacecraft attitude control system at the main modes under disturbances and digital control of the gyro moment clusters by the few-excessive gyrodine schemes.


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    Title :

    Attitude guidance, navigation and robust control of an agile land-survey satellite


    Contributors:


    Publication date :

    2017-06-01


    Size :

    507331 byte




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



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