Global search for low-thrust transfers to the Moon in the planar circular restricted three-body problem
Global search for low-thrust transfers to the Moon in the planar circular restricted three-body problem
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DOI：
10.1007/s10569-016-9748-2
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发表时间：
2017-02
影响因子：
1.6
通讯作者：
K. Oshima;S. Campagnola;Tomohiro Yanao
中科院分区：
文献类型：
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作者：
K. Oshima;S. Campagnola;Tomohiro Yanao
本文在平面、圆形、限制性三体问题中，对小推力月球转移进行了全局搜索。采用间接法计算推进剂质量最优轨迹，该方法基于庞特里亚金原理实现了最优性的必要条件。我们提出的技术，以减少所需的初始costates搜索集的维数。我们获得了广泛的帕累托解决方案的飞行时间和质量消耗。使用Tisserand-Poincaré图，显示了一些解决方案，以利用高海拔月球飞越，以减少燃料消耗。
This paper globally searches for low-thrust transfers to the Moon in the planar, circular, restricted, three-body problem. Propellant-mass optimal trajectories are computed with an indirect method, which implements the necessary conditions of optimality based on the Pontryagin principle. We present techniques to reduce the dimension of the set over which the required initial costates are searched. We obtain a wide range of Pareto solutions in terms of time of flight and mass consumption. Using the Tisserand–Poincaré graph, a number of solutions are shown to exploit high-altitude lunar flybys to reduce fuel consumption.