Path: SC/BasicOrbit
% Computes the true anomaly from the mean anomaly without wrapping. Between -pi / pi -------------------------------------------------------------------------- Form: nu = M2NuAbs( e, M, tol, nMax ) -------------------------------------------------------------------------- ------ Inputs ------ e Eccentricity M Mean anomaly (rad) tol Tolerance (optional) nMax Maximum number of iterations (optional) ------- Outputs ------- nu True anomaly (rad) --------------------------------------------------------------------------
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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