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Bi-elliptic Transfer Between Coplanar Circular Orbits

version 1.1 (492 KB) by

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

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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.

Comments and Ratings (2)

Rebecca Yap

sun Chong

Updates

1.1

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

MATLAB Release
MATLAB 7.14 (R2012a)

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