Low Energy Transfer to the Moon

By Wang Sang Koon, Martin W. Lo, Jerrold E. Marsden, Shane D. Ross. 2001

388 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Astronomy and Astrophysics

View Paper: https://www.semanticscholar.org/paper/08ca14ad2ea332ed6fe64248d2ac5ea7cda5327e

How researchers see this paper

The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.

In Aerospace Engineering

1. Josep J. Masdemont
2. Jerrold E. Marsden
3. Wang Sang Koon
4. Shane D. Ross
5. Martin W. Lo
6. Otto van Koert
7. Urs Frauenfelder

In Astronomy and Astrophysics

1. Josep J. Masdemont
2. Jerrold E. Marsden
3. Wang Sang Koon
4. Shane D. Ross
5. Martin W. Lo
6. Francesco Topputo
7. Otto van Koert
8. Urs Frauenfelder

Citations in the corpus

• Invariant Manifolds, the Spatial Three-Body Problem and Space Mission Design (2001, methodology): “Extending Results from Planar Model to Spatial Model Previous work based on the planar circular restricted three-body problem (PCR3BP) revealed the basic structures controlling the dynamics.(4,5,6,7) But future missions will require three-dimensional capabilities, such as control of the latitude and”
• Advanced global optimisation for mission analysis and design (2004, background): “The Sun/Earth/Moon/Spacecraft 4 body system can be effectively approximated as two coupled 3 body systems [28].”
• On optimal two-impulse Earth–Moon transfers in a four-body model (2013, background): “Analogously, the second part (i.e. the lunar ballistic capture) is an orbit defined inside the stable manifold of the periodic orbits about L2 in the Earth–Moon problem (Gómez et al. 2001; Koon et al. 2001; Parker 2006; Parker and Lo 2006).”