Path: SC/BasicOrbit
% Eccentric anomaly for an ellipse. Computed from the mean anomaly and the eccentricity. The user can optionally specify a tolerance and maximum number of iterations. For a demo plot call M2EEl( ecc ). -------------------------------------------------------------------------- Form: eccAnom = M2EEl( ecc, meanAnom, tol, nMax ) or eccAnom = M2EEl( ecc, meanAnom, tol ) or eccAnom = M2EEl( ecc, meanAnom) -------------------------------------------------------------------------- ------ Inputs ------ ecc (1,:) Eccentricity meanAnom (1,:) Mean anomaly tol (1,1) Tolerance(optional, default is 1e-8) nMax (1,1) Maximum number of iterations (optional, default is no maximum. Can only be input if tol is also specified.) ------- Outputs ------- eccAnom (1,:) Eccentric anomaly --------------------------------------------------------------------------
SC: BasicOrbit/M2EApp Common: CommonData/SwooshWatermark Common: General/CellToMat Common: General/MatToCell Common: General/Watermark Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle Math: Linear/DupVect
Back to the SC Module page