Single Impulse De-orbit
Version 1.0.0.0 (339 KB) by
David Eagle
Two MATLAB scripts that be used to compute the characteristics of single impulse de-orbit maneuvers.
PDF document and MATLAB scripts for computing the characteristics of single impulsive maneuvers required to de-orbit from circular and elliptical Earth orbits. These scripts also provide simple graphic displays of the de-orbit trajectory.
Cite As
David Eagle (2026). Single Impulse De-orbit (https://uk.mathworks.com/matlabcentral/fileexchange/39177-single-impulse-de-orbit), MATLAB Central File Exchange. Retrieved .
MATLAB Release Compatibility
Created with
R2011a
Compatible with any release
Platform Compatibility
Windows macOS LinuxCategories
Find more on Visualization in Help Center and MATLAB Answers
Tags
Discover Live Editor
Create scripts with code, output, and formatted text in a single executable document.
| Version | Published | Release Notes | |
|---|---|---|---|
| 1.0.0.0 |
