Trans-Lunar Trajectory Optimization - OTB/MICE version

Version 1.0.4 (30.5 MB) by David Eagle
Optimization Toolbox version of the tlto_matlab script used to design preliminary lunar missions from Earth park orbit to B-plane encounter.
307 Downloads
Updated 15 Jul 2021

View License

This submission is a MATLAB script named tlto_matlab_otb 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 - OTB/MICE version (https://www.mathworks.com/matlabcentral/fileexchange/73600-trans-lunar-trajectory-optimization-otb-mice-version), MATLAB Central File Exchange. Retrieved .

MATLAB Release Compatibility
Created with R2019b
Compatible with any release
Platform Compatibility
Windows macOS Linux

Community Treasure Hunt

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

Start Hunting!
Version Published Release Notes
1.0.4

Updated several algorithms (apparent sidereal time, sun/moon ephemeris) and the PDF documentation.

1.0.3

Distribution now includes an OTB version (tlto_mice_otb.zip) that uses JPL MICE routines for computing ephemerides.

1.0.2

Added node/apse alignment targeting option. Updated documentation.

1.0.1

Bug fix and documentation update.

1.0.0