Optimal earth–moon trajectories in elliptic models: part 2 transfer between elliptic low earth orbit to elliptic low moon orbit-Reference-Cited by-同舟云学术

Optimal earth–moon trajectories in elliptic models: part 2 transfer between elliptic low earth orbit to elliptic low moon orbit

Published:2022-05 Issue:5 Volume:44 Page:
ISSN:1678-5878
Container-title:Journal of the Brazilian Society of Mechanical Sciences and Engineering
language:en
Short-container-title:J Braz. Soc. Mech. Sci. Eng.

Author:

Gagg Filho Luiz Arthur^ORCID,da Silva Fernandes Sandro

Publisher

Springer Science and Business Media LLC

Subject

Mechanical Engineering,General Engineering,Aerospace Engineering,Automotive Engineering,Industrial and Manufacturing Engineering,Applied Mathematics

Link

https://link.springer.com/content/pdf/10.1007/s40430-022-03504-z.pdf

Reference22 articles.

1. Alessi EM, Buzzoni A, Daquin J, Carbognani A, Tommei G (2021) Dynamical properties of the Molniya satellite constellation: long-term evolution of orbital eccentricity. Acta Astronautica 179:659–669, https://doi.org/10.1016/j.actaastro.2020.11.047, arXiv:2007.04341

2. Bate RR, Mueller DD, White JE (1971) Fundamentals of Astrodynamics. Courier Dover Publications, New York

3. Belbruno EA, Miller JK (1993) Sun-perturbed Earth-to-moon transfers with ballistic capture. J Guidance Control Dyn 16(4):770–775. https://doi.org/10.2514/3.21079

4. da Silva Fernandes S, Gagg Filho LA (2021) Optimal Earth-Moon trajectories in elliptic models: part 1 round-trip missions. J Brazilian Soc Mech Sci Eng 43(12):1–27. https://doi.org/10.1007/s40430-021-03281-1, https://link.springer.com/article/10.1007/s40430-021-03281-1

5. Da Silva Fernandes S, Marinho CMP (2013) Sun perturbations on optimal trajectories for earth-moon flight. In: Proceedings..., International Congress of Mechanical Engineering COBEM 2013, ABCM, Rio de Janeiro