ArticleA semi-analytical solution for the motion of a low altitude Earth satellite under J2-gravity and air drag perturbations
ArticleA semi-analytical solution for the motion of a low altitude Earth satellite under J2-gravity and air drag perturbations
ArticleTHE EFFECT OF THE EARTH'S OBLATENESS AND ATMOSPHERIC DRAG ON AN ARTIFICIAL SATELLITE IN TERMS OF THE EULER PARAMETERS
ArticleTHE EFFECT OF THE EARTH'S OBLATENESS AND ATMOSPHERIC DRAG ON AN ARTIFICIAL SATELLITE IN TERMS OF THE EULER PARAMETERS
ArticleEclipses intervals for satellites in elliptical orbit under effects of solar radiation pressure and earth’s oblatness
ArticleEclipses intervals for satellites in elliptical orbit under effects of solar radiation pressure and earth’s oblatness
ArticleThe effects of an artificial radial acceleration on the positions of L4 and L5 and their stability in the restricted three-body Problem
ArticleThe effects of an artificial radial acceleration on the positions of L4 and L5 and their stability in the restricted three-body Problem