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。
Based on the multi-impulse method of orbit maneuvers, the method to enable the whole satellite formation to maneuver with micro-propulsion thrusters was studied in this paper.
基于多冲量轨道机动控制，研究应用微小推力发动机来实现卫星编队轨道机动控制的方法。
A general solution for multi impulse maneuvers in space rendezvous is derived.
导出了空间交会中多脉冲变轨的一般算法。
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