Multiobjective genetic optimization of Earth–Moon trajectories in the restricted four-body problem-Reference-Cited by-同舟云学术

Multiobjective genetic optimization of Earth–Moon trajectories in the restricted four-body problem

Published:2010-02 Issue:3 Volume:45 Page:398-409
ISSN:0273-1177
Container-title:Advances in Space Research
language:en
Short-container-title:Advances in Space Research

Author:

Assadian Nima,Pourtakdoust Seid H.

Publisher

Elsevier BV

Subject

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

Reference44 articles.

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2. Andreu, M.A. The quasi-bicircular problem, PhD Dissertation, University of Barcelona, 1998.

3. Dynamics of capture in the restricted three-body problem;Astakhov;Astronomical Society of the Pacific Conference Series, Order and Chaos in Stellar and Planetary Systems,2004

4. Fundamentals of Astrodynamics;Bate,1971

5. Sun-perturbed Earth-to-Moon transfers with ballistic capture;Belbruno;J. Guid. Contr. Dyn.,1993

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