Transfer orbits in the restricted problem

Details Transfer orbits in the restricted problem Transfer orbits in the restricted problem

Nov 1994

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1994stin...9616862p&link_type=abstract

Presented at the AIAA Astrodynamics Conference, Scottsdale, AZ, 1-3 Aug. 1994

Astronomy and Astrophysics

Astronomy

Lagrangian Equilibrium Points, Orbital Mechanics, Space Transportation, Three Body Problem, Transfer Orbits, Earth-Moon System, Equations Of Motion, Jacobi Integral, Numerical Integration, Orbit Calculation, Swingby Technique

Scientific paper

This paper studies transfer orbits in the planar restricted three-body problem. In particular, we are searching for orbits that can be used in two situations: (1) to transfer a spacecraft from one body back to the same body, known in the literature as the Henon's problem; and (2) to transfer a spacecraft from one body to the respective Lagrangian points L(sub 4) and L(sub 5). To avoid numerical problems during close approaches the global Lamaitre regularization is used. Under this model, the Henon's problem became a Lambert's three body problem, as defined and explained in this paper.

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