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Orbit Design for Lunar Polar Region Exploration
- ZHOU Wenyan1, GAO Shan1, LIU Decheng1, ZHANG Xiangyu1, MA Jinan1, YU Dengyun2
Author information
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1. Beijing Institute of Spacecraft System Engineering,Beijing 100094,China;
2. China Aerospace Science and Technology Corporation,Beijing 100048,China
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History
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Received |
Revised |
09 Nov 2019 |
21 Apr 2020 |
Issue Date |
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20 May 2022 |
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References
[1] SCHMID E P. Lunar far-side communication satellites[R]. Greenbelt,MD,United States:NASA,1968.
[2] 高珊,周文艳,张磊,等. 嫦娥四号中继星任务轨道设计与实践[J]. 中国科学:技术科学,2019,49(2):156-165
GAO S,ZHOU W Y,ZHANG L,et al. Trajectory design and flight results for Chang’e-4 relay satellite[J]. Scientia Sinica Technologica,2019,49(2):156-165
[3] HAMERA K,MOSHER T,GEFREH M. An evolvable lunar communication and navigation constellation concept[C]//2008 IEEE Aerospace Conference. Big Sky,MT,USA:IEEE,2008.
[4] BRUNNER W C. Conceptual design of a communications relay satellite for a lunar sample return mission[C]//43rd AIAA Aerospace Sciences Meeting and Exhibit. Reno,Nevada:AIAA,2005.
[5] DAVIS D,BHATT S,HOWELL K. Orbit maintenance and navigation of human spacecraft at cislunar near rectilinear Halo orbits[R]. USA:AIAA,2017.
[6] 杨维廉. 月球卫星的冻结轨道[J]. 宇航学报,2008,29(2):426-429
YANG W L. Forzen orbit of the lunar satellite[J]. Journal of Astronautics,2008,29(2):426-429
[7] ELY A T. Coverage and control of constellations of elliptical inclined frozen lunar orbits[C]//2005 AAS/AIAA Astrodynamics Specialist Conference. Pasadena,CA:AIAA,2005.