A Rotors Spin-up and Checking a Switching on the Redundant Controlling Gyro Cluster into Spacecraft Attitude Control System

The method for a rotors spin up and the bringing of redundant controlling gyro cluster to its park state without creation of disturbing torques during the spacecraft angular stabilization is suggested and studied. We present the research results on checking the gyro cluster switching on into the attitude control system for a space robot and a land-surveying satellite in sun-synchronous orbit.