EME2000 to/from True-of-Date Transformation
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 (2024). 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 .
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- MATLAB > External Language Interfaces > Other languages > SPICE files >
- MATLAB > Mathematics > Computational Geometry > Cartesian Coordinate System Conversion >
- Physical Modeling > Simscape Electrical > Electrical Block Libraries > Semiconductors and Converters >
- Aerospace > Aerospace Toolbox > Standard Workflow Procedures > Unit Conversions >
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Version | Published | Release Notes | |
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1.0.0.0 |