Evolution of orbital characteristics in the case of the restricted elliptical three-body problem at first-order commensurability.
A restricted version of the three-body planet problem has been considered. In the case of first-order commensurability the analytical solution for an insignificant eccentricity has been found. This solution describes the evolution of all orbital characteristics of a passively gravitating body. Researches described cover internal and external versions of the problem.
- Pub Date:
- Evolution (Development);
- Orbit Calculation;
- Orbital Elements;
- Orbital Mechanics;
- Three Body Problem;
- Astronomical Models;
- Mathematical Models;
- Three-Body Problem: Restricted;
- Three-Body Problem: Orbital Evolution