Ephemeris calculations with mice in matlab

The following Matlab project contains the source code and Matlab examples used for ephemeris calculations with mice. This MATLAB script calculates the state vector of the Moon as seen from the Earth in the J2000 frame at the DE405 integration epoch using MICE routines (naif.jpl.nasa.gov/naif/toolkit_MATLAB.html).

The source code and files included in this project are listed in the project files section, please make sure whether the listed source code meet your needs there.

Project Files: 

File NameSize
cspice_deltet.m 5590
cspice_et2utc.m 6141
cspice_furnsh.m 3794
cspice_unload.m 4418
de405_integration_epoch.m 1583
de405_integration_epoch.txt 322
license.txt 1311
mice_spkezr.m 18047
naif0010.tls 5068
zzmice_dp.m 2669
zzmice_int.m 4720
zzmice_str.m 3341