Nu2M:

Path: SC/BasicOrbit

% Converts true anomaly to mean anomaly.

--------------------------------------------------------------------------
   Form:
   [meanAnom,eccAnom] = Nu2M( e, nu )
--------------------------------------------------------------------------

   ------
   Inputs
   ------
   e             (1,1)  Eccentricity
   nu            (1,:)  True anomaly

   -------
   Outputs
   -------
   meanAnom       (1,:)  Mean anomaly
   eccAnom        (1,:)  Eccentric anomaly

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

Children:

SC: BasicOrbit/E2M
SC: BasicOrbit/Nu2E
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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