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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 (2026). Circular Orbit Plane Change (https://www.mathworks.com/matlabcentral/fileexchange/39178-circular-orbit-plane-change), MATLAB Central File Exchange. Retrieved .
General Information
- Version 1.1.0.0 (217 KB)
MATLAB Release Compatibility
- Compatible with any release
Platform Compatibility
- Windows
- macOS
- Linux
