Secular perturbations of nearly parabolic orbits of comets

Computer Science

Scientific paper

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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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