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.
卫星轨道控制期间，轨道控制推力会激振挠性太阳帆板，从而也影响卫星的姿态。
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.
卫星轨道控制期间，轨道控制推力会激振挠性太阳帆板，从而也影响卫星的姿态。
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