Moon Position
Version 2.2.0 (94.8 MB) by
Meysam Mahooti
Position of the Moon referred to the mean equator and equinox of J2000
Five different approaches are used in the test_MoonPosition.m for the computation of lunar coordinates; NASA JPL Development Ephemerides (DE440), very accurate ELP2000-82, high-precision analytical series (Brown's theory), low-precision analytical series, and Simpson analytical method.
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).
Cite As
Meysam Mahooti (2026). Moon Position (https://in.mathworks.com/matlabcentral/fileexchange/56041-moon-position), MATLAB Central File Exchange. Retrieved .
MATLAB Release Compatibility
Created with
R2024a
Compatible with any release
Platform Compatibility
Windows macOS LinuxCategories
Find more on Gravitation, Cosmology & Astrophysics in Help Center and MATLAB Answers
Tags
Discover Live Editor
Create scripts with code, output, and formatted text in a single executable document.
Moon Position
| Version | Published | Release Notes | |
|---|---|---|---|
| 2.2.0 | test_MoonPosition.m was modified. |
||
| 2.1.1 | JPL Developement Ephemerides DE436 was replaced by DE440, and Mjday.m was modified. |
||
| 2.1.0.0 | The DE436 full matrix is added. |
||
| 2.0.0.0 | JPL Development Ephemerides (DE430) is replaced by DE436. |
||
| 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 | Description is updated.
. |
