NASA JPL Development Ephemerides (DE405)
バージョン 2.0.0 (53 MB) 作成者:
Meysam Mahooti
DE405 covers 1599-12-09 to 2201-02-20. Referred to the International Celestial Reference Frame.
The JPL planetary ephemerides are saved as files of Chebyshev polynomials fit to the Cartesian positions and velocities of the planets, the Sun, and the Moon, typically in 32-day intervals. The positions are integrated in astronomical units (au), but with polynomials stored in units of kilometers.
References:
Standish, E.M.: 1998, "JPL Planetary and Lunar Ephemerides, DE405/LE405",JPL IOM 312.F-98-048.
引用
Meysam Mahooti (2024). NASA JPL Development Ephemerides (DE405) (https://www.mathworks.com/matlabcentral/fileexchange/54842-nasa-jpl-development-ephemerides-de405), MATLAB Central File Exchange. に取得済み.
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