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.
随着小卫星应用领域的日益广阔和小卫星数量的不断增长，对小卫星轨道控制技术的要求也越来越高。
With the wide application of small satellite and its increasing quantity, the requirements for orbit control technology of the small satellite is becoming more strict.
届时地面控制人员将点燃助推器，把卫星送入预定轨道。
Ground controllers will then fire the booster, sending the satellite into its proper orbit.
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