Bi-elliptic Transfer Between Coplanar Circular Orbits
Bi-elliptic orbital transfer between two coplanar circular Earth orbits.
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This 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.
Cite As
David Eagle (2026). 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 .
Acknowledgements
Inspired: BiEllipticOrbitTransfer Tool With GUI
General Information
- Version 1.2.0.0 (433 KB)
MATLAB Release Compatibility
- Compatible with any release
Platform Compatibility
- Windows
- macOS
- Linux
