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Circular Orbit Plane Change

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Circular Orbit Plane Change

by David Eagle

 

27 Nov 2012 (Updated 18 Jul 2013)

MATLAB script for solving the circular orbit plane change problem.

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Description

This document presents the geometry and equations associated with the single impulse maneuver that modifies the inclination and/or right ascension of the ascending node (RAAN) of circular orbits. It also describes a MATLAB script that solves this classic astrodynamic problem.

MATLAB release MATLAB 7.14 (R2012a)
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Updates
18 Jul 2013

Added three-dimensional display of orbits. Updated PDF document.

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