Secular perturbations of elements in the restricted parabolic three-body problem
Abstract
Analytical formulas are obtained for secular perturbations of the eccentricity and of the pericenter argument in the restricted parabolic three-body problem. The perturbations obtained are compared with the results of numerical integration of twice-averaged equations. The results can be used to describe the evolution of planets in a planetary system.
- Publication:
-
Astronomicheskii Zhurnal
- Pub Date:
- December 1991
- Bibcode:
- 1991AZh....68.1323M
- Keywords:
-
- Motion Stability;
- Perturbation Theory;
- Three Body Problem;
- Analytic Functions;
- Numerical Integration;
- Parabolas;
- Secular Variations;
- Astrophysics