The propulsionsubsystem is essential for maneuvering the MUOS satellite during transfer orbit to its final location as well as conducting on-orbit repositioning maneuvers throughout its mission life.
在把MUOS卫星变轨到最终位置以及执行任务寿命期内的在轨机动性重新配置上，该推进系统是很关键的。
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The theory of integrated fire/flight/propulsion control(IFFPC) and the control law of its subsystem were studied in this paper.