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:
Folkner, W. M., et al. (2014). The planetary and lunar ephemerides DE430 and DE431.
引用格式
Meysam Mahooti (2025). NASA JPL Development Ephemerides (DE430) (https://www.mathworks.com/matlabcentral/fileexchange/60504-nasa-jpl-development-ephemerides-de430), MATLAB Central File Exchange. 检索时间: .
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版本 | 已发布 | 发行说明 | |
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2.0.0 | It was revised on November 23, 2024. |
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1.1.1.0 | The DE430 full matrix is added. |
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1.1.0.0 | test_JPL430eph.m is modified. |
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1.0.0.1 | Title is changed. |
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1.0.0.0 |
for i=1:2285
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