Fig. 1. Decoupling control law and manipulation law for the satellite attitude control scheme

Fig. 2. Attitude maneuver predictive control scheme considering the SGCMG characteristics

Fig. 3. Configurationof the 4-SGCMG pyramid

Fig. 4. Simulation results of the attitude maneuver prediction controller

Fig. 5. Results of the attitude maneuvering by the control law

Fig. 6. Resultsof the attitude maneuvering simulation with the 3-SGCMG （PID）

Fig. 7. Simulation results of the 3-SGCMG predictive control