Acceleration of gyrorotors and switching on a redundant gyrodine cluster in a loop for attitude control of information satellite

We have suggested and studied the method for acceleration of gyrorotors and to bring the gyrodine cluster to its park state without the creation of disturbing torques during angular stabilization of the satellite body by a propulsion unit. We have presented the research results on processes of acceleration the gyrodine rotors, the bringing the gyro moment cluster into the park and its switching on in a loop for the attitude control of an information satellite in sun-synchronous orbit.