Design and analysis of quasi-halo orbits and optimal transfers from the Earth under different Sun–Earth frameworks using differential evolution

Author:

Neelakantan RithwikORCID,Ramanan R. V.

Publisher

Springer Science and Business Media LLC

Subject

Space and Planetary Science,Astronomy and Astrophysics

Reference29 articles.

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2. Campagnola S., Lo M., Newton P. 2008, Advances in the Astronautical Sciences, 130, 1541

3. Dunham D. W. Jen S. J., Roberts C. E., et al. 1992, in Transfer trajectory design for the SOHO libration-point mission (Washington, DC: International Astronautical Federation Congress)

4. Farquhar R. W., Muhonen D., Richardson D. 1976. Mission design for a halo orbiter of the Earth. Astrodynamics Conference, 810

5. Farquhar R. W. 1971, The utilization of halo orbits in advanced lunar operations. National Aeronautics and Space Administration, Vol. 6365

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