Path: SC/BasicOrbit
% Computes the eccentric anomaly from the mean anomaly and the eccentricity. -------------------------------------------------------------------------- Form: eccAnom = M2E( e, meanAnom, tol, nMax ) -------------------------------------------------------------------------- ------ Inputs ------ e (1,:) Eccentricity meanAnom (1,:) Mean anomaly (rad) tol (1,1) Tolerance nMax (1,1) Maximum number of iterations ------- Outputs ------- eccAnom (1,:) Eccentric anomaly (rad) --------------------------------------------------------------------------
SC: BasicOrbit/M2EApp SC: BasicOrbit/M2EEl SC: BasicOrbit/M2EHy 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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