Averaged parabolic restricted three-body problem
Abstract
The plane, singly averaged parabolic restricted three-body problem is considered. The expansion of the perturbing function is obtained in the case when the first two terms are taken. Results of the numerical integration of the exact and singly averaged equations are presented. Element variations are considered for the case of Mars.
- Publication:
-
Astronomicheskii Zhurnal
- Pub Date:
- April 1989
- Bibcode:
- 1989AZh....66..377M
- Keywords:
-
- Orbit Perturbation;
- Parabolic Flight;
- Three Body Problem;
- Computational Astrophysics;
- Numerical Integration;
- Astrophysics