Astronomy and Astrophysics – Astronomy
Scientific paper
Feb 2006
adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2006cemda..94..135k&link_type=abstract
Celestial Mechanics and Dynamical Astronomy, Volume 94, Issue 2, pp.135-153
Astronomy and Astrophysics
Astronomy
2
Doubly Asymptotic Periodic Orbits, Heteroclinic Orbits, Homoclinic Orbits, Oblateness, Restricted Three-Body Problem
Scientific paper
Asymptotic motion to collinear equilibrium points of the restricted three-body problem with oblateness is considered. In particular, homoclinic and heteroclinic solutions to these points are computed. These solutions depart asymptotically from an equilibrium point and arrive asymptotically at the same or another equilibrium point and are important reference solutions. To compute an asymptotic orbit, we use a fourth order local analysis, numerical integration and standard differential corrections.
Douskos C. N.
Kalantonis V. S.
Perdios E. A.
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