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SUPPORT SITE |
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SUPPORT SITE |
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Path: SC/BasicOrbit
% Generate the eccentric anomaly from the mean anomaly and the eccentricity. Since version 1. -------------------------------------------------------------------------- Form: eccAnom = M2E( e, meanAnom, tol, nMax ) -------------------------------------------------------------------------- ------ Inputs ------ e (: or 1) Eccentricity meanAnom (:) Mean anomaly tol (1,1) Tolerance nMax (1,1) Maximum number of iterations ------- Outputs ------- eccAnom (:) Eccentric anomaly --------------------------------------------------------------------------
Common: Graphics/Plot2D Math: Linear/DupVect SC: BasicOrbit/M2EEl SC: BasicOrbit/M2EHy
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