This paper mainly discuss the problem of method and policy of spacecraft's large scale orbital maneuver.
论文研究了航天器大范围轨道机动的方法与策略。
With the development of space mobile platform application, the orbital maneuver technology has been becoming the focus research.
随着空间平台相关应用的推进，其轨道机动技术已经成为研究的重点。
The attitude control law is designed for the orbital maneuver with considering the output character of the attitude control 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。
A new intelligent planning algorithm which is used for fixed-time, point-to-point, multi-impulse orbital maneuver in the two-body problem is proposed in this paper.
针对二体轨道模型，设计了一种时间固定点对点多冲量轨道机动的智能规划算法。
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。
According to the requirements of our Earth observation satellite's orbital maneuver mission, this paper designs and implements the software module and primary program for orbital maneuver.
针对我国对地观测小卫星的轨道机动任务要求，该文设计了轨道机动的软件模块和主要程序。
After the taikonauts had returned to Earth, the BX-1 was placed under active control and commanded to maneuver back towards the orbital module, which had been left in orbit.
宇航员返回地球之后，BX - 1实施了主动控制，并通过命令向留在轨道上的轨道舱返回。
After the taikonauts had returned to Earth, the BX-1 was placed under active control and commanded to maneuver back towards the orbital module, which had been left in orbit.
宇航员返回地球之后，BX - 1实施了主动控制，并通过命令向留在轨道上的轨道舱返回。
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