Author: Kalantonis V. Douskos C. Perdios E.
Publisher: Springer Publishing Company
ISSN: 0923-2958
Source: Celestial Mechanics and Dynamical Astronomy, Vol.94, Iss.2, 2006-02, pp. : 135-153
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Abstract
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.
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