Trans-Lunar Trajectory Optimization - SNOPT/MICE versions

Version 1.2.0 (58.2 MB) by David Eagle
SNOPT version of the tlto_matlab script used to design preliminary lunar missions from Earth park orbit to B-plane encounter.
156 Downloads
Updated 12 Jun 2021

View License

This submission is a MATLAB script named tlto_matlab that can be used to design preliminary lunar missions from Earth park orbit to B-plane encounter at the moon. The software assumes trans-lunar injection (TLI) occurs impulsively from a circular Earth park orbit. The B-plane coordinates used for targeting the final conditions at the moon are expressed in a moon-centered (selenocentric) mean equator and IAU node of epoch coordinate system. The results from this scientific simulation can be used as an initial guess for a finite-burn trajectory optimization program.

Cite As

David Eagle (2024). Trans-Lunar Trajectory Optimization - SNOPT/MICE versions (https://www.mathworks.com/matlabcentral/fileexchange/74321-trans-lunar-trajectory-optimization-snopt-mice-versions), MATLAB Central File Exchange. Retrieved .

MATLAB Release Compatibility
Created with R2019b
Compatible with any release
Platform Compatibility
Windows macOS Linux
Categories
Find more on Coordinate Systems in Help Center and MATLAB Answers

Community Treasure Hunt

Find the treasures in MATLAB Central and discover how the community can help you!

Start Hunting!
Version Published Release Notes
1.2.0

Distribution now includes a version (tlto_mice_snopt.zip) that uses JPL MICE routines to evaluate the de430.bsp ephemerides.

1.1.0

Added node/apsis alignment targeting. Updated documentation.

1.0.0