A MATLAB Script for Designing Interplanetary Launch Trajectories

Version 1.0.0.0 (362 KB) by David Eagle
Preliminary design and analysis of interplanetary launch trajectories.
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Updated 12 Nov 2012

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This MATLAB script determines the launch universal time, orbital elements of the departure hyperbola, injection delta-v, and estimates park orbit coast times for both short and long coast injection opportunities. This information can be used to create initial guesses for other trajectory simulations.

Cite As

David Eagle (2024). A MATLAB Script for Designing Interplanetary Launch Trajectories (https://www.mathworks.com/matlabcentral/fileexchange/39008-a-matlab-script-for-designing-interplanetary-launch-trajectories), MATLAB Central File Exchange. Retrieved .

MATLAB Release Compatibility
Created with R2011a
Compatible with any release
Platform Compatibility
Windows macOS Linux
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Version Published Release Notes
1.0.0.0