Circular Orbit Plane Change

MATLAB script for solving the circular orbit plane change problem.
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Updated 18 Jul 2013

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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.

Cite As

David Eagle (2024). Circular Orbit Plane Change (https://www.mathworks.com/matlabcentral/fileexchange/39178-circular-orbit-plane-change), MATLAB Central File Exchange. Retrieved .

MATLAB Release Compatibility
Created with R2012a
Compatible with any release
Platform Compatibility
Windows macOS Linux
Categories
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Version Published Release Notes
1.1.0.0

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

1.0.0.0