Design and analysis of a direct transfer trajectory from a near rectilinear halo orbit to a low lunar orbit-Reference-Cited by-同舟云学术

Design and analysis of a direct transfer trajectory from a near rectilinear halo orbit to a low lunar orbit

Published:2021-02 Issue:3 Volume:67 Page:1143-1154
ISSN:0273-1177
Container-title:Advances in Space Research
language:en
Short-container-title:Advances in Space Research

Author:

Lu Lin,Li Haiyang,Zhou Wanmeng,Liu Jianghui

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Space and Planetary Science,Aerospace Engineering,General Earth and Planetary Sciences,Atmospheric Science,Geophysics,Astronomy and Astrophysics

Reference35 articles.

1. Blazquez, E., Beauregard, L., Lizy-Destrez, S., 2018. Safe natural far rendezvous approaches for cislunar near rectilinear halo orbits in the ephemeris model, in: 7th International Conference on Astrodynamics Tools and Techniques, Oberpfaffenhofen, Germany.

2. Rendezvous in lunar near rectilinear halo orbits;Bucci;Adv. Astronaut. Sci. Technol.,2018

3. Bucci, L., Lavagna, M., Jehn, R., 2017. Station keeping techniques for near rectilinear orbits in the Earth–Moon system, in: Proceedings of 10th International ESA Conference on GNC Systems, Salzburg, Austria.

4. Carlos, S.L., Cuartielles, S., Pau, J., 2018. Near rectilinear orbits around the moon as operational orbit for the future deep space gateway, in: 7th International Conference on Astrodynamics Tools and Techniques, Oberpfaffenhofen, Germany.

5. Chavers, G., Suzuki, N., Smith, M., et al., 2019. NASA’s human lunar landing strategy, in: 70th International Astronautical Congress, Washington D.C., United States of America.

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