ORBIT MAINTENANCE AND NAVIGATION OF HUMAN SPACECRAFT AT CISLUNAR NEAR RECTILINEAR HALO ORBITS

被引：0

作者：

Davis, Diane C. ^{[1
]}

Bhatt, Sagar A. ^{[2
]}

Howell, Kathleen C. ^{[3
]}

Jang, Jiann-Woei ^{[2
]}

Whitley, Ryan J. ^{[4
]}

Clark, Fred D. ^{[2
]}

Guzzefti, Davide ^{[5
]}

Zimovan, Emily M. ^{[5
]}

Barton, Gregg H. ^{[2
]}

机构：

[1] Ai Solut Inc, Houston, TX 77058 USA

[2] Charles Stark Draper Labs Inc, Houston, TX 77058 USA

[3] Purdue Univ, Sch Aeronaut & Astronaut, Aeronaut & Astronaut, 701 West Stadium Ave, W Lafayette, IN 47907 USA

[4] NASA JSC, Explorat Miss Planning Off, Houston, TX 77058 USA

[5] Purdue Univ, Sch Aeronaut & Astronaut, 701 West Stadium Ave, W Lafayette, IN 47907 USA

来源：

SPACEFLIGHT MECHANICS 2017, PTS I - IV | 2017年 / 160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：

Multiple studies have concluded that Earth-Moon libration point orbits are attractive candidates for staging operations. The Near Rectilinear Halo Orbit (NRHO), a member of the Earth-Moon halo orbit family, has been singularly demonstrated to meet multi-mission architectural constraints. In this paper, the challenges associated with operating human spacecraft in the NRHO are evaluated. Navigation accuracies and human vehicle process noise effects are applied to various stationkeeping strategies in order to obtain a reliable orbit maintenance algorithm. Additionally, the ability to absorb missed burns, construct phasing maneuvers to avoid eclipses and conduct rendezvous and proximity operations are examined.

引用

页码：2257 / 2276

页数：20

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