EME2000 to/from True-of-Date Transformation

Version 1.0.0.0 (24.7 KB) by David Eagle
This Matlab script converts between true-of-date and EME2000 state vectors using Mice routines.
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Updated 30 Nov 2012

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This Matlab script can be used to transform between Earth-centered inertial (ECI) true-of-date Cartesian coordinates and the corresponding coordinates in the Earth mean equator and equinox of J2000 (EME2000) coordinate system. The software is based on several MATLAB versions of the SPICE library routines provided by JPL (http://naif.jpl.nasa.gov/naif/).

Cite As

David Eagle (2025). EME2000 to/from True-of-Date Transformation (https://www.mathworks.com/matlabcentral/fileexchange/39147-eme2000-to-from-true-of-date-transformation), 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