Solution set calculation of the Sun-perturbed optimal two-impulse trans-lunar orbits using continuation theory-Reference-Cited by-同舟云学术

Solution set calculation of the Sun-perturbed optimal two-impulse trans-lunar orbits using continuation theory

Published:2020-02-29 Issue:1 Volume:4 Page:75-86
ISSN:2522-008X
Container-title:Astrodynamics
language:en
Short-container-title:Astrodyn

Author:

He Bo-yong,Shen Hong-xin

Publisher

Springer Science and Business Media LLC

Subject

Space and Planetary Science,Astronomy and Astrophysics,Aerospace Engineering

Link

https://link.springer.com/content/pdf/10.1007/s42064-020-0069-6.pdf

Reference25 articles.

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2. Gill, T. NASA’s lunar orbital platform-Gateway. In: Proceedings of the 45th Space Congress, 2018.

3. Bureau, E. T. India’s moonshot: All about Chandrayaan-2. Available at http://econimicstime.indiatimes.com/news/science/indias-moonshot-all-about-chandrayaan-2/articleshow/70338414.cms (cited 23 July 2019).

4. Topputo, F. On optimal two-impulse Earth-Moon transfers in a four-body model. Celestial Mechanics and Dynamical Astronomy, 2013, 117(3): 279–313.

5. Gong, S. P., Li, J. F., Baoyin, H. X., Gao, Y. F. Lunar landing trajectory design based on invariant manifold. Applied Mathematics and Mechanics, 2007, 28(2): 201–207.

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