Stability of periodic orbits in the elliptic, restricted three-body problem.
Author:
Affiliation:
1. Jet Propulsion Laboratory, Pasadena, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.5267
Reference6 articles.
1. On changes of independent variable in dynamical systems and applications to regularization
2. The computation of characteristic exponents in the planar restricted problem of three bodies
3. Szebehely, V., Theory of Orbits; theRestricted Problem of Three Bodies, Academic Press, New York, 1967, pp.587-602.
4. Periodic Orbits.
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