A lunar flyby for a tridimensional Earth-to-Earth mission-Reference-Cited by-同舟云学术

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A lunar flyby for a tridimensional Earth-to-Earth mission

Published:2018-10 Issue: Volume:151 Page:228-242
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Gagg Filho Luiz Arthur^ORCID,da Silva Fernandes Sandro^ORCID

Funder

São Paulo Research Foundation

CNPq

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference26 articles.

1. The celestial mechanics of gravity assist;Broucke,1988

2. Trajectories for flyby sample return at saturn's moons;Jones,2016

3. Trajectories for europa flyby sample return;Jones,2016

4. Fast reconnaissance missions to the outer solar system utilizing energy derived from the gravitational field of jupiter1;Flandro;Astronaut. Acta,1966

5. Interplanetary trajectory optimization with application to galileo;D'Amario;J. Guid. Contr. Dynam.,1982

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1. Powered lunar flyby for transfers between non-coplanar orbits around Earth;Advances in Space Research;2023-11

2. Bayesian Optimization of crewed lunar free return abort trajectory;Acta Astronautica;2022-12

3. Optimal earth–moon trajectories in elliptic models: part 2 transfer between elliptic low earth orbit to elliptic low moon orbit;Journal of the Brazilian Society of Mechanical Sciences and Engineering;2022-05

4. A SURVEY ON EXTENSIONS OF THE PURE GRAVITY SWING-BY MANEUVER;Revista Mexicana de Astronomía y Astrofísica;2021-10-01

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