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Low-Energy Earth-to-Halo Transfers in the Earth–Moon Scenario with Sun-Perturbation

  • Anna Zanzottera
  • Giorgio Mingotti
  • Roberto Castelli
  • Michael Dellnitz
Chapter

Abstract

In this work, trajectories connecting LEOs with halos around libration points of the Earth–Moon CRTBP are investigated. Suitable first guess solutions are searched linking together the stable manifolds of the halo orbits (of the EM spatial CRTBP) with the Earth-departing trajectories (built in the SE planar CRTBP). As a first step, small discontinuities, in terms of Δv are allowed and bounded through the box-covering approach, implemented with the software GAIO. Then, the first guess solutions are optimized in the bicircular four-body problem: single-impulse and two-impulse transfers are presented and discussed.

Keywords

Stable Manifold Libration Point Halo Orbit Parking Orbit Collinear Libration Point 
These keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves.

Notes

Acknowledgements

This work was supported by the Marie Curie Actions Research and Training Network AstroNet, Contract Grant No. MCRTN-CT-2006-035151.

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Copyright information

© Springer Science+Business Media, LLC 2011

Authors and Affiliations

  • Anna Zanzottera
    • 1
  • Giorgio Mingotti
  • Roberto Castelli
  • Michael Dellnitz
  1. 1.Dipartimento di Matematica F.BrioschiMilanoItaly

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