Optimal low-thrust transfers to halo orbits about the L2 libration point in the Earth-Moon system (elliptical problem)

被引：0
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作者：
Starchville, TF
Melton, RG
机构：
来源：
SPACEFLIGHT MECHANICS 1998, VOL 99, PTS 1 AND 2 | 1998年 / 99卷
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暂无
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
This paper develops a systematic procedure for generating optimal low-thrust transfers from one of the primaries in the elliptic restricted three-body problem (ER3BP) to a halo orbit in the three-body system. The examples all involve transfers from Earth to halo orbits about the L2 point in the Earth-Moon system. Using a transformation to the pulsating coordinate system (distances scaled by the time-varying range between primaries), it is possible to employ the method of stable manifolds to determine low-thrust trajectories that correctly inject into a specified halo orbit. The paper includes examples of both circular and elliptical halo orbits.
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页码：1489 / 1505
页数：17
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