Path: SC/BasicOrbit
% Computes the mean anomaly from the true anomaly without wrapping btwn -pi / pi -------------------------------------------------------------------------- Form: M = Nu2MAbs( e, nu, tol, nMax ); -------------------------------------------------------------------------- ------ Inputs ------ e Eccentricity nu True anomaly (rad) tol Tolerance (optional) nMax Maximum number of iterations (optional) ------- Outputs ------- M Mean anomaly (rad) --------------------------------------------------------------------------
SC: BasicOrbit/E2M SC: BasicOrbit/Nu2E SC: BasicOrbit/Nu2M 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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