A survey of different classes of Earth-to-Moon trajectories in the patched three-body approach

Author:

de Sousa-Silva Priscilla A.,Terra Maisa O.

Funder

CAPES (Brazil)

FAPESP (Brazil)

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference31 articles.

1. Dynamical Systems, The Three-Body Problem, and Space Mission Design;Koon,2006

2. Artemis mission design;Sweetser;Space Sci. Rev.,2011

3. M. Chung, S. Hatch, J. Kangas, S. Long, R. Roncoli, T. Sweetser, Trans-lunar cruise trajectory design of GRAIL (Gravity Recovery and Interior Laboratory) mission, in: AIAA/AAS Astrodynamics Specialist Conference, AIAA, 2010, paper ID AIAA 2010-8384, http://dx.doi.org/10.2514/6.2010-8384.

4. Connecting orbits and invariant manifolds in the spatial restricted three-body problem;Gómez;Nonlinearity,2004

5. E. Belbruno, J. Miller, A Ballistic Lunar Capture Trajectory for the Japanese Spacecraft Hiten, Technical Report 312/90.4-1731-EAB, Jet Propulsion Laboratory, 1990.

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