Abstract: The multi-objective optimization model for the attitude control of the flexible satellite was constructed,and a multi-objective optimization elitist evolutionary algorithm was applied to the path planning for large angle maneuver of flexible satellite,in order to further improve the performance of the attitude control system.Simulation results indicate that the proposed approach could find a diverse set of non-dominated path solutions efficiently in one run,whereby the decision maker can make a choice in the case of different working requirements.Meanwhile,the conflicts among criterions of rapidity,stability degree of the attitude and low vibration of solar panel caused by maneuver of the satellite can be alleviated.