M2Nu:

Path: SC/BasicOrbit

% Computes the true anomaly from the mean anomaly.

   Since version 1.
--------------------------------------------------------------------------
   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)

--------------------------------------------------------------------------

Children:

Common: Graphics/Plot2D
SC: BasicOrbit/E2Nu
SC: BasicOrbit/M2E
SC: BasicOrbit/M2NuPb

Back to the SC Module page