Bi-elliptic Transfer Between Coplanar Circular Orbits

Version 1.1.0.0 (492 KB) von David Eagle
Bi-elliptic orbital transfer between two coplanar circular Earth orbits.
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Aktualisiert 9. Jul 2013

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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.

Zitieren als

David Eagle (2024). 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. Abgerufen .

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Erstellt mit R2012a
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Version Veröffentlicht Versionshinweise
1.1.0.0

Added three-dimensional trajectory graphics and a graphical primer vector analysis. Updated PDF document to reflect these new features.
1.0.0.0