STABILITY ANALYSIS IN THE RESTRICTED FOUR BODY PROBLEM WITH OBLATNESS AND RADIATION PRESSURE.

STABILITY ABOUT LIBRATION POINTS FOR RESTRICTED FOUR-BODY PROBLEM

NUMERICAL SOLUTION OF SATELLITE MOTION UNDER THE EFFECTS OF THE EARTH’S GRAVITY OF THE AXIAL SYMMETRY AND DRAG FORCE IN TERMS OF THE KS-REGULARIZED VARIABLES

PERTURBED GROUND TRACK UNDER THE INFLUENCE OF J2 AND LUNISOLAR FORCES

STUDYING STABILITY OF THE LIBERATION POINTS OFBINARY ASTEROIDES

A semi-analytical solution for the motion of a low altitude Earth satellite under J2-gravity and air drag perturbations

THE EFFECT OF THE EARTH'S OBLATENESS AND ATMOSPHERIC DRAG ON AN ARTIFICIAL SATELLITE IN TERMS OF THE EULER PARAMETERS

On the Location of The Lagrangian Collinear Points In The Photo-Gravitational Relativistic Restricted 3-Body Problem

Eclipses intervals for satellites in elliptical orbit under effects of solar radiation pressure and earth’s oblatness

On the Orbital Stability of Pendulum-Like Vibration of a Rigid Body Carrying a Rotor