Path: SC/BasicOrbit
% Computes the true anomaly from the mean anomaly. -------------------------------------------------------------------------- Form: nu = M2Nu( e, M, tol, nMax ) -------------------------------------------------------------------------- ------ Inputs ------ e (1,1) Eccentricity M (1,:) Mean anomaly (rad) tol (1,1) Tolerance nMax (1,1) Maximum number of iterations ------- Outputs ------- nu (1,:) True anomaly (rad) --------------------------------------------------------------------------
SC: BasicOrbit/E2Nu SC: BasicOrbit/M2E SC: BasicOrbit/M2EApp SC: BasicOrbit/M2EEl SC: BasicOrbit/M2EHy 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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