On optimal two-impulse Earth-Moon transfers in a four-body model

被引:126
作者
Topputo, Francesco [1 ]
机构
[1] Politecn Milan, Dept Aerosp Sci & Technol, I-20156 Milan, Italy
关键词
Earth-Moon transfer; Low-energy transfer; Ballistic capture; Trajectory optimization; Restricted three-body problem; Restricted four-body problem; WEAK STABILITY BOUNDARY; LOW-ENERGY; OPTIMAL TRAJECTORIES; INVARIANT-MANIFOLDS; BALLISTIC ESCAPE; CAPTURE; OPTIMIZATION; SPACECRAFT;
D O I
10.1007/s10569-013-9513-8
中图分类号
P1 [天文学];
学科分类号
0704 ;
摘要
In this paper two-impulse Earth-Moon transfers are treated in the restricted four-body problem with the Sun, the Earth, and the Moon as primaries. The problem is formulated with mathematical means and solved through direct transcription and multiple shooting strategy. Thousands of solutions are found, which make it possible to frame known cases as special points of a more general picture. Families of solutions are defined and characterized, and their features are discussed. The methodology described in this paper is useful to perform trade-off analyses, where many solutions have to be produced and assessed.
引用
收藏
页码:279 / 313
页数:35
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