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ArticleThe effects of an artificial radial acceleration on the positions of L4 and L5 and their stability in the restricted three-body Problem
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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
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