Path: SC/Ephem
% Generate the moon position in the earth-centered inertial frame. Uses SunV1 -------------------------------------------------------------------------- Form: r = RMoonECI( jD ) -------------------------------------------------------------------------- ------ Inputs ------ jD (1,:) Julian date ------- Outputs ------- r (3,:) Moon vector --------------------------------------------------------------------------
SC: Ephem/MoonV1 Common: Time/Date2JD
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