Abstract
The paper deals with the problems on further development of a rational strategy for the space robot's approaching a geostationary satellite and visual checking its state. Original methods are proposed for predicting the influence of gravitational disturbances, as well as solar pressure forces in the synthesis of the robot guidance laws for its interorbital flights. The developed methods and algorithms for a space robot control are based on the local optimizing the fuel consumption of the plasma electric propulsion unit. Simulation results on developed guidance and control algorithms are presented that demonstrate their effectiveness.
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