Stability Analysis of Elliptical Restricted Three Body Problem

Zusatztext

The study here is for the equilibrium position of the primaries with the infinitesimal body. In particular, the possible positions of the equilibrium occurred when the three bodies form an equilateral triangle. The application of this model can be seen in the motion of Trojan - asteroids. The asteroids are only influenced by the gravitational forces of the Sun and Jupiter, and the orbit of Jupiter around Sun is assumed to be a fixed ellipse.

Autorenportrait

Dr. Krishna Kumar pandey completed M.Sc( Mathematics) in the year 2006 from Govt. Science College Durg(C.G), India. He has Completed M.Phil in 2011 and Ph.D in July 2019 from Dr C.V. Raman University, Kota, Bilaspur(C.G), India.he is Working as Assistant Professor in the Department of Mathematics

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