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Bi-elliptic Transfer Between Coplanar Circular Orbits

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Bi-elliptic Transfer Between Coplanar Circular Orbits

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02 Nov 2012 (Updated )

Bi-elliptic orbital transfer between two coplanar circular Earth orbits.

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Description

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.

Required Products MATLAB
MATLAB release MATLAB 7.14 (R2012a)
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10 Jun 2014 sun Chong  
Updates
09 Jul 2013

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

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