The problems of approaching a space robot to a geostationary satellite and visual checking its technical state are considered. The robot’s control system uses a plasma electric propulsion unit, a propulsion unit based on eight catalytic electric reaction engines with pulse-width modulation of thrust and a gyroscopic moment cluster based on four single-gimbal control moment gyroscopes – gyrodines. Simulation results using the developed guidance and control algorithms are presented, which demonstrate their effectiveness in accuracy.


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    Title :

    Analysis of the Space Robot Control Accuracy at Checking a Geostationary Satellite State


    Contributors:


    Publication date :

    2022-06-27


    Size :

    2901685 byte





    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English




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