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Moon Position

version 1.1.0.0 (17.9 MB) by Meysam Mahooti
Position of the Moon referred to the mean equator and equinox of J2000

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Updated 26 Jan 2018

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Five different approaches are used in the test_MoonPos.m for the computation of lunar coordinates; NASA JPL Development Ephemerides (DE430), very accurate ELP2000-82, high-precision analytical series (Brown's theory), Simpson analytical method and low-precision analytical series.
References:
1. Montenbruck O., Gill E.; Satellite Orbits: Models, Methods and Applications; Springer Verlag, Heidelberg; Corrected 3rd Printing (2005).
2. Montenbruck O., Pfleger T.; Astronomy on the Personal Computer; Springer Verlag, Heidelberg; 4th edition (2000).
3. Vallado D. A; Fundamentals of Astrodynamics and Applications; McGraw-Hill; New York; 3rd edition(2007).
4. van Flandern T. C., Pulkkinen K. F.; Low precision formulae for planetary positions; Astrophysical Journal Supplement Series 41, 391 (1979).
5. http://ssd.jpl.nasa.gov/?ephemerides
6. http://www.astro.caltech.edu/~eran/MATLAB/EphemCon.html
7. https://celestrak.com/SpaceData/

Comments and Ratings (7)

Updates

1.1.0.0

Ephemeris Time (ET) is introduced as the best approximation of Barycentric Dynamical Time (TDB) and Terrestrial Time (TT) for prediction purposes. Moreover, very accurate ELP2000-82 lunar coordinates is computed.

1.0.0.0

.

1.0.0.0

Revised on 2016-12-17.

1.0.0.0

Description is updated.

MATLAB Release Compatibility
Created with R2017b
Compatible with any release
Platform Compatibility
Windows macOS Linux