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.
Analysis of the Space Robot Control Accuracy at Checking a Geostationary Satellite State
2022-06-27
2901685 byte
Conference paper
Electronic Resource
English
Bentham Science Publishers | 2022
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