Periodic orbits around the collinear liberation points in the restricted three body problem when the smaller primary is a triaxial rigid body : Sun-Earth case

Astronomy and Astrophysics – Astronomy

Scientific paper

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Restricted Three-Body Problem, Triaxial Rigid Body, Periodic Orbits, Liapunov Stability

Scientific paper

Periodic orbits belonging to the Stromgren families A, B and C around
the collinear liberation points in the restricted three body problem
have been studied when the smaller primary is a triaxial rigid body by
taking different values of semiaxes of the triaxial rigid body. The
Liapunov stability of each periodic solution has also been examined.

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