EME2000 to/from True-of-Date Transformation

版本 1.0.0.0 (24.7 KB) 作者: David Eagle
This Matlab script converts between true-of-date and EME2000 state vectors using Mice routines.
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更新时间 2012/11/30

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This Matlab script can be used to transform between Earth-centered inertial (ECI) true-of-date Cartesian coordinates and the corresponding coordinates in the Earth mean equator and equinox of J2000 (EME2000) coordinate system. The software is based on several MATLAB versions of the SPICE library routines provided by JPL (http://naif.jpl.nasa.gov/naif/).

引用格式

David Eagle (2024). EME2000 to/from True-of-Date Transformation (https://www.mathworks.com/matlabcentral/fileexchange/39147-eme2000-to-from-true-of-date-transformation), MATLAB Central File Exchange. 检索来源 .

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版本 已发布 发行说明
1.0.0.0