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。
Introduce the reference frame and time system used in orbit design particularly. Analyzed the orbit characteristic of two-body problem and launch window.
详细介绍了用于轨道设计的坐标系统和时间系统,分析了二体轨道特性和发射窗口的基本特性。
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