GLOBAL SEARCH FOR LOW-ENERGY TRANSFERS TO THE MOON WITH LONG TRANSFER TIME

被引:0
作者
Oshima, Kenta [1 ]
Topputo, Francesco [2 ]
Yanao, Tomohiro [1 ]
机构
[1] Waseda Univ, Dept Appl Mech & Aerosp Engn, Tokyo 1698555, Japan
[2] Politecn Milan, Dept Aerosp Sci & Technol, I-20156 Milan, Italy
来源
SPACEFLIGHT MECHANICS 2017, PTS I - IV | 2017年 / 160卷
关键词
INVARIANT-MANIFOLDS; GRAVITY ASSISTS; TRAJECTORIES; CAPTURE; LUNAR; OPTIMIZATION; ESCAPE;
D O I
暂无
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The present paper globally searches for two-impulse, low-energy transfers to the Moon in the planar bicircular restricted four-body problem with transfer time up to 200 days. A grid search combined with a direct transcription and multiple shooting technique reveals numerous families of optimal low-energy solutions. We investigate characteristics of solutions in terms of two- and three-body parameters, and discuss a trade-off between time and cost (Delta v) by exploring Pareto-optimal solutions, considering the presence or absence of lunar gravity assist. Analyzing orbital characteristics based on multi-body dynamics, we show useful perturbations of the Sun, Earth, and Moon to reduce Delta v.
引用
收藏
页码:577 / 594
页数:18
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