Periodic orbits of the second kind in the restricted three-body problem when the more massive primary is an oblate spheroid |
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| Authors: | Ram Krishan Sharma |
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| Institution: | (1) Applied Mathematics Section, Aeronautics Group, Vikram Sarabhai Space Centre, Trivandrum, India |
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| 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. |
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