The problem of guidance and attitude control for a land-survey satellite at a scanning stereoscopic imagery is considered. The synthesis of the satellite angular guidance law is based on relations that bind the image motion with the kinematic parameters of the satellite spatial motion relative to the Earth’s surface, ensuring constant values of the observation distance and angle of convergence during a scanning from two perspectives. We present the developed methods and the results of the simulation of the stereoscopic imagery fulfilled by a satellite in a sun-synchronous orbit.


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    Title :

    Land-survey satellite guidance and attitude control when a scanning stereoscopic imagery


    Contributors:

    Conference:

    ICNPAA 2018 WORLD CONGRESS: 12th International Conference on Mathematical Problems in Engineering, Aerospace and Sciences ; 2018 ; Yerevan, Armenia


    Published in:

    Publication date :

    2018-12-04


    Size :

    7 pages





    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



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