NEAR RECTILINEAR HALO ORBITS AND THEIR APPLICATION IN CIS-LUNAR SPACE

被引：0
|
作者：
Zimovan, Emily M. [1 ,2 ,3 ]
Howell, Kathleen C. [3 ,4 ]
Davis, Diane C. [2 ,5 ]
机构：
[1] Purdue Univ, Sch Aeronaut & Astronaut, Armstrong Hall Engn, 701 W Stadium Ave, W Lafayette, IN 47907 USA
[2] AAS, Washington, DC 20006 USA
[3] AIAA, Reston, VA 20191 USA
[4] Purdue Univ, Sch Aeronaut & Astronaut, Armstrong Hall Engn, 701 W Stadium Ave, W Lafayette, IN 47907 USA
[5] Ai Solutions Inc, 2224 Bay Area Blvd, Houston, TX 77058 USA
来源：
THIRD IAA CONFERENCE ON DYNAMICS AND CONTROL OF SPACE SYSTEMS 2017 | 2017年 / 161卷
关键词：
D O I：
暂无
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
Near Rectilinear Halo Orbits (NRHOs), a subset of the L-1 and L-2 halo orbit families, are strong candidates for a future inhabited facility in cis-lunar space. Characteristics of the NRHOs, including stability and eclipsing properties, are presented along with a strategy to detect real-time diverging behavior. To be useful to future missions, the accessibility of these orbits must also be addressed. Transfer options from the NRHOs to the Distant Retrograde Orbits (DROs) are investigated. Additionally, a brief overview of past NRHO stationkeeping analysis is included.
引用
收藏
页码：209 / 228
页数：20
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