EME2000 to/from True-of-Date Transformation
This Matlab script converts between true-of-date and EME2000 state vectors using Mice routines.
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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 (2026). 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 .
General Information
- Version 1.0.0.0 (24.7 KB)
MATLAB Release Compatibility
- Compatible with any release
Platform Compatibility
- Windows
- macOS
- Linux
| Version | Published | Release Notes | Action |
|---|---|---|---|
| 1.0.0.0 |
