Using the continuation method we prove that the circular and the elliptic symmetric periodic orbits of the planar rotating Kepler problem can be continued into periodic orbits of the planar collision restricted 3-body problem. Additionally, we also continue to this restricted problem the so called "comet orbits". © Springer Science+Business Media B.V. 2006.
- Collision restricted 3-body problem
- Continuation method
- Periodic orbits