Path: SC/Ephem
% Generate the sun position in the earth-centered inertial frame. Uses SunV1 -------------------------------------------------------------------------- Form: r = RSunECI( jD ) -------------------------------------------------------------------------- ------ Inputs ------ jD (1,:) Julian date ------- Outputs ------- r (3,:) Sun vector --------------------------------------------------------------------------
SC: Ephem/SunV1 Common: Time/DTSToDTA Common: Time/Date2JD Math: Linear/Mag Math: Linear/Unit Math: Trigonometry/CosD Math: Trigonometry/SinD
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