Path: Orbit/OrbitCoord
% Computes the ECI position of the Earth-Moon Barycenter. Uses MoonV1 for ephemeris and Constant to look up the gravitational parameters. -------------------------------------------------------------------------- Form: b = BarycenterEarthMoon( jD ) -------------------------------------------------------------------------- ------ Inputs ------ jD (1,:) Julian date (days) ------- Outputs ------- b (3,:) Barycenter --------------------------------------------------------------------------
AC: ACData/ACTConstants SC: BasicOrbit/RVFromKepler SC: Ephem/MoonV1 SC: SCData/sCTConstants Common: CommonData/Constants Common: CommonData/SwooshWatermark Common: CommonData/xSplashSmall Common: Database/Constant Common: General/CellToMat Common: General/DeBlankLT Common: General/DeleteCell Common: General/MatToCell Common: General/Watermark Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/Plot3D Common: Graphics/PltStyle Common: Graphics/TimeLabl Common: Graphics/XLabelS Common: Graphics/YLabelS Common: Graphics/ZLabelS Common: Time/DTSToDTA Common: Time/Date2JD Common: Time/JD2000 Math: Linear/Mag Math: Linear/Unit Math: Trigonometry/CosD Math: Trigonometry/SinD
Back to the Orbit Module page