This is a MATLAB script that can be used to determine the characteristics of a three impulse bi-elliptic transfer between two coplanar circular orbits. The impulsive assumption means that the velocity, but not the position, of the space vehicle is changed instantaneously.
Added three-dimensional trajectory graphics and a graphical primer vector analysis. Updated PDF document to reflect these new features.
Download apps, toolboxes, and other File Exchange content using Add-On Explorer in MATLAB.