Path: SCPro/ProEphemeris
% Computes eclipses from time and ECI position. Utilizes the low-precision sun ephemeris in SunV1. -------------------------------------------------------------------------- Form: n = EclipseFromECI(r, t, jD0, a) -------------------------------------------------------------------------- ------ Inputs ------ r (3,:) Position vector of the spacecraft t (1,:) Time vector jD0 (1,1) Initial Julian date a (1,:) Auxiliary input to plot ------- Outputs ------- n (1,:) Normalized sun intensity ( 0 < n < 1 ) -------------------------------------------------------------------------- See also: SunV1, Eclipse --------------------------------------------------------------------------
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: Ephem/Eclipse SC: Ephem/SunV1 Common: CommonData/SwooshWatermark Common: General/CellToMat Common: General/DeBlankLT Common: General/MatToCell Common: General/Watermark Common: Graphics/Axis3D Common: Graphics/Mesh2 Common: Graphics/NPlot 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 Common: Time/JD2000 Math: Linear/Dot Math: Linear/DupVect Math: Linear/Mag Math: Linear/Unit Math: Trigonometry/CosD Math: Trigonometry/SinD
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