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.
David Eagle (2022). Bi-elliptic Transfer Between Coplanar Circular Orbits (https://www.mathworks.com/matlabcentral/fileexchange/38885-bi-elliptic-transfer-between-coplanar-circular-orbits), MATLAB Central File Exchange. Retrieved .
MATLAB Release Compatibility
Platform CompatibilityWindows macOS Linux
Inspired: BiEllipticOrbitTransfer Tool With GUI
Community Treasure Hunt
Find the treasures in MATLAB Central and discover how the community can help you!Start Hunting!