We investigated the motion of an infinitesimal mass and the Sun-Earth elliptic restricted three-body problem with radiation effect in this paper. The perturbation technique was used to obtain semi-analytic expressions for the location of collinear points, and the influence of radiation on collinear points was investigated. To investigate the stability of triangle points, critical mass expressions based on the radiative primary are used. The Jacobi constant ‘C,’ as well as Zero Velocity Curves, were also discovered.

Author (S) Details

Dr. Avaneesh Vaishwar
Department of Mathematics, MCAET Akbarpur, Ambedkar Nagar-224122, Uttar Pradesh, India.

View Book :- https://stm.bookpi.org/CTMCS-V2/article/view/1776

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