Optimization of low-thrust transfers in the three body problem

被引：0
|
作者：
A. A. Sukhanov
A. F. B. de A. Prado
机构：
[1] Russian Academy of Sciences,Space Research Institute
[2] Instituto Nacional de Pesquisas Espaciais (INPE),undefined
来源：
Cosmic Research | 2008年 / 46卷
关键词：
45.40. Gj;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
We consider transfers with low thrust in an arbitrary field of forces. The modified method of transporting trajectory [1–4] is used for optimization of the transfers. The complexity of finding the transporting trajectory of a preset type can be the main obstacle to application of this method. This challenge is solved for the three-body problem in the Hill motion model. Numerical analysis of the method is performed using an example of the transfers to halo-orbits around the solar-terrestrial libration points.
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页码：413 / 424
页数：11
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