Co-simulating Study on Flexible Support Control Moment Gyroscope Machine, Electricity, Magnetism and Control

Aiming at the problem that the control performance of the frame system will become worse and even lose stability after the control moment gyroscope is installed on the vibration isolation platform, this paper conducts co-simulation based on ADAMS, ANSYS and MATLAB to study the Kinematics and dynamics of the control moment gyroscope under different flexible support conditions. The results of the paper can be used to simulate the operation of control torque gyroscopes under various conditions such as multiple operating conditions, variable loads, variable damping, variable stiffness, and zero gravity. Reverse guidance is provided for the design of isolation platforms and control torque gyroscopes, which has important engineering application significance for achieving low disturbance and high-precision control performance of control torque gyroscopes, and thus achieving high-precision control performance of spacecraft attitude.