Optimal transfers from Moon to <mml:math xmlns:mml="http://www.w3.org/1998/Math/MathML" altimg="si83.svg"><mml:mrow><mml:msub><mml:mrow><mml:mi>L</mml:mi></mml:mrow><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msub></mml:mrow></mml:math> halo orbit of the Earth-Moon system-Reference-Cited by-同舟云学术

Optimal transfers from Moon to L2 halo orbit of the Earth-Moon system

Published:2022-12 Issue:11 Volume:70 Page:3362-3372
ISSN:0273-1177
Container-title:Advances in Space Research
language:en
Short-container-title:Advances in Space Research

Author:

Santos L.B.T.,Sousa-Silva P.A.,Terra M.O.,Mani Karthik V.,de Almeida A.K.,Sanchez D.M.,Prado A.F.B.A.

Publisher

Elsevier BV

Subject

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

Reference43 articles.

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2. Bosanac, N., 2012. Exploring the influence of a three-body interaction added to the gravitational potential function in the circular restricted three-body problem: A numerical frequency analysis. Master’s thesis Purdue University, Indiana.

3. Mission analysis for the em-1 cubesats equuleus and omotenashi;Campagnola;IEEE Aerosp. Electron. Syst. Mag.,2019

4. Orbit Design for LUMIO: the Lunar Meteoroid Impacts Observer;Cipriano;Front. Astron. Space Sci.,2018

5. Dei Tos, D.A., 2018. Trajectory optimization of limited control authority spacecraft in high-fidelity models. Ph.D. thesis. https://doi.org/10.13140/RG.2.2.15099.00804.

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