关键词: 挠性卫星，大角度机动，姿态控制，多目标优化，进化算法

Abstract: The attitude control for large angle maneuver of flexible satellite requires the satellite can follow the given angle quickly. Meanwhile, vibration of solar panel caused by maneuver of the satellite is expected to be low. A new multi-objective optimization evolutionary algorithm was applied to the path planning for large angle maneuver of satcllife, which can optimize both the rapidity of maneuver and low vibration of solar panel. Simulation results indicate that the proposed approach can search a diverse set of non-dominated path solutions in one run efficiently, from which the decision maker can make a selection under different working requirements. I}he approach proposed alleviates the confhcts between two criteria.

Key words: Flexible satellite, Large angel maneuver, Attitude control, Multi objective optimization, Evolutionary algorithms