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日-地(月)系拉格朗日L1点及晕(Halo)轨道应用

Application of Lagrange L1 Point and Halo Orbits in Sun-Earth(Moon) System
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摘要 日-地(月)系统拉格朗日L1点及L1点附近的晕(Halo)轨道在"夸父"工程中有重要的应用价值,可用于对太阳实施持续观测。利用数值分析方法,找到了日-地(月)-探测器三者构成的圆限制性三体问题中L1点附近的周期晕(Halo)轨道,分析了轨道的特性。研究结果对"夸父"工程中的目标轨道设计有一定的参考价值。 Lagrange L1 Point and Halo Orbits aound it in Sun-Earth(Moon) System play an important role in "Kuafu" project. Halo Orbits around L1 point can be used in continuous sun observation. This paper computes periodic Halo orbits around L1 point in circular-restricted three bodies problem, composed of Sun-Earth(Moon)-Probe, by means of numerical analytical method, and researchs the feature of these Halo orbits. The results are useful for target orbit design of "Kuafu" project.
出处 《火力与指挥控制》 CSCD 北大核心 2009年第11期133-135,共3页 Fire Control & Command Control
基金 高等学校博士学科专项科研基金资助项目(200606990241)
关键词 拉格朗日点 晕(Halo)轨道 圆限制性三体问题 微分校正 lagrange point, Halo orbit, circular-restricted three bodies problem, differential correction
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