Path: Orbit/OrbitCoord
% Converts orbital elements to commonly used angular quantities Since version 1. -------------------------------------------------------------------------- Form: [L, K, l] = El2LKl( el ) -------------------------------------------------------------------------- ------ Inputs ------ el Elements vector [a,i,W,w,e,M] ------- Outputs ------- L True longitude ( w + W + f ) K Eccentric longitude ( w + W + E ) l Mean longitude ( w + W + M ) --------------------------------------------------------------------------
SC: BasicOrbit/E2Nu SC: BasicOrbit/M2E SC: BasicOrbit/M2EApp SC: BasicOrbit/M2EEl SC: BasicOrbit/M2EHy SC: BasicOrbit/M2Nu SC: BasicOrbit/M2NuPb Common: CommonData/SwooshWatermark Common: General/CellToMat Common: General/MatToCell Common: General/Watermark Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle Math: Linear/DupVect
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