The attitudecontrol law is designed for the orbital maneuver with considering the output character of the attitudecontrol thrusters.
根据姿态控制推力器的输出特性，设计了轨道控制期间卫星姿态控制方案。
2
When the satellite takes orbital maneuver, the control force may stimulate the vibration of the flexible appendages and, therefore, affects the attitude of the satellite.