Path: SCPro/ProEphemeris
% Computes the moon ECI elements Uses the state of the moon from a single epoch to compute elements. Type MoonECIElements for a comparison with MoonV1 and MoonV2. -------------------------------------------------------------------------- Form: [el, jD] = MoonECIElements -------------------------------------------------------------------------- ------ Inputs ------ None ------- Outputs ------- el (1,6) [a i W w e M] jD (1,1) Epoch of elements -------------------------------------------------------------------------- Reference: JPL Horizons, https://ssd.jpl.nasa.gov/horizons.cgi (2020) --------------------------------------------------------------------------
Orbit: OrbitCoord/SLR Orbit: OrbitMechanics/RVOrbGen SC: BasicOrbit/CP2I SC: BasicOrbit/E2M SC: BasicOrbit/E2Nu SC: BasicOrbit/M2E SC: BasicOrbit/M2EApp SC: BasicOrbit/M2EEl SC: BasicOrbit/M2EHy SC: BasicOrbit/Nu2E SC: BasicOrbit/Nu2M SC: BasicOrbit/RV2El SC: Ephem/MoonV1 SC: Ephem/MoonV2 Common: CommonData/SwooshWatermark Common: General/CellToMat Common: General/DeBlankLT Common: General/MatToCell Common: General/Watermark Common: Graphics/Axis3D Common: Graphics/Mesh2 Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle Common: Graphics/TimeLabl Common: Graphics/XLabelS Common: Graphics/YLabelS Common: Graphics/ZLabelS Common: Time/DTSToDTA Common: Time/Date2JD Math: Linear/Cross Math: Linear/DupVect Math: Linear/Mag Math: Linear/Unit Math: Trigonometry/CosD Math: Trigonometry/SinD
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