Ejection-Collision Orbits with the More Massive Primary in the Planar Elliptic Restricted Three Body Problem

Details Ejection-Collision Orbits with the More Massive Primary in the Planar Elliptic Restricted Three Body Problem Ejection-Collision Orbits with the More Massive Primary in the Planar Elliptic Restricted Three Body Problem

Dec 1995

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1995cemda..61..315p&link_type=abstract

Celestial mechanics and dynamical astronomy, Volume 61, Issue 4, pp.315-331

Astronomy and Astrophysics

Astronomy

Ejection-Collision Orbits, Restricted Three Body Problem, Regularization

Scientific paper

The main goal of this paper is to give an approximation to initial conditions for ejection-collision orbits with the more massive primary, in the planar elliptic restricted three body problem when the mass parameter µ and the eccentricity e are small enough. The proof is based on a regularization of variables and a perturbation of the two body problem.

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