Abstract: Fast maneuver of flexible satellite system often requires large attitude changing with reduction of vibration. In this paper, pulse sequence control methodology is presented based on unconstrained mode equations to suppress residual vibration; besides, pulse sequence programming is proposed to minimize maneuvering time. The methods can meet the requirements of the fast maneuver and without residual vibration after maneuvering. Moreover, it is very suitable to satellite systems equipped with on off jets and reaction wheels. Finally, numeric simulation is explored to verify the validity of pulse sequence control.