Computer Science
Scientific paper
Oct 1992
adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1992kfnt....8...82e&link_type=abstract
Kinematika i Fizika Nebesnykh Tel (ISSN 0233-7665), vol. 8, no. 5, p. 82-88.
Computer Science
2
Comets, Orbit Perturbation, Orbital Mechanics, Solar Orbits, Perihelions, Three Body Problem
Scientific paper
The secular evolution of nearly parabolic orbits of comets under the attraction of several planets moving in circular complanar orbits is considered. The method of investigation is based on the analytical expansion for the secular part of the disturbing function in the restricted three-body problem. The behavior of integral curves is studied qualitatively and quantitatively in the range of perihelion distances which are typical for observed comets.
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