SGP4
Citation pour cette source
Meysam Mahooti (2024). SGP4 (https://www.mathworks.com/matlabcentral/fileexchange/62013-sgp4), MATLAB Central File Exchange. Récupéré le .
Compatibilité avec les versions de MATLAB
Plateformes compatibles
Windows macOS LinuxCatégories
- Aerospace > Aerospace Blockset > Reference Applications >
- Sciences > Earth, Ocean, and Atmospheric Sciences > Earth and Planetary Science >
- Engineering > Aerospace Engineering > Satellite and Orbital Mechanics >
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Remerciements
A inspiré : epoch2datevec(tle_epoch)
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SGP4
SGP4_Vectorized
Version | Publié le | Notes de version | |
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2.1.1 | test_sgp4.m was modified. |
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2.1.0 | The vectorized SGP4 package was added. |
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2.0.1 | satdata.xndt2o in test_sgp4.m was corrected. |
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2.0.0 | Mjday.m was modified. |
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1.1.1.0 | test_sgp4.m is modified. |
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1.1.0.0 | Satellite's state vector is computed in four different coordinate systems, i.e. Earth-centered inertial (ECI), Earth-centered Earth-fixed (ECEF), true of date (TOD) and true equator mean equinox (TEME). |
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1.0.0.0 | . |