Abstract
Utilizing secular perturbing potential due to oblateness, the existence of periodic orbits of the second kind is established through analytic continuation using Delaunay's canonical variables in the planar restricted three-body problem when the more massive primary is an oblate spheroid with its equatorial plane coincident with the plane of motion.
References
Arenstorf, R. F.: 1963,Am. J. Math. 85, 27.
Barrar, R. B.: 1965,Astron. J. 70, 3.
Giacaglia, G. E. O.: 1967,Astron. J. 72, 386.
Sharma, R. K.: 1976,Astron. Astrophys. 50, 257.
Stiefel, E. L. and Scheifele, G.: 1971,Linear and Regular Celestial Mechanics, Springer Verlag.
Szebehely, V.: 1967,Theory of Orbits, Academic Press.
Author information
Authors and Affiliations
Rights and permissions
About this article
Cite this article
Sharma, R.K. Periodic orbits of the second kind in the restricted three-body problem when the more massive primary is an oblate spheroid. Astrophys Space Sci 76, 255–258 (1981). https://doi.org/10.1007/BF00651258
Received:
Issue Date:
DOI: https://doi.org/10.1007/BF00651258