Abstract
Near a symmetric periodic orbit of the plane circular or elliptic restricted probelm, the conditions for a symmetric periodic orbit of the plane general three body problem are reduced, under a natural nondegeneracy condition, to the vanishing of a single real valued function. The implicit function theorem and Hörmander's generalized Morse's lemma are then used to analyze the set of zeros of this function.
Similar content being viewed by others
References
Bozis, G. and Hadjidemetriou, J. D.: 1976,Celest. Mech. 13, 127–136.
Broucke, R.: 1969,AIAA J. 7, 1003–1009.
Hadjidemetriou, J. D.: 1975,Celest. Mech. 12, 155–174.
Hadjidemetriou, J. D. and Christides, Th.: 1975,Celest. Mech. 12, 175–188.
Hörmander, L.: 1971,Acta Math. 127, 79–183.
Kammeyer, P. C.: 1974, Thesis, New York University.
Siegel, C. L. and Moser, J. K.: 1971,Lectures on Celestial Mechanics, Springer-Verlag, New York.
Szebehely, V. G.: 1967,Theory of Orbits, Academic Press, New York.
Author information
Authors and Affiliations
Rights and permissions
About this article
Cite this article
Kammeyer, P.C. Periodic three body orbits in the case of small third mass. Celestial Mechanics 17, 121–125 (1978). https://doi.org/10.1007/BF01371323
Received:
Issue Date:
DOI: https://doi.org/10.1007/BF01371323