M2NuS:

Path: Orbit/OrbitCoord

% Computes true anomaly from a series expansion

   Since version 1.
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   Form:
   nu = M2NuS( e, M )
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   ------
   Inputs
   ------
   e                     Eccentricity
   M              (1,:)  Mean anomaly (rad)

   -------
   Outputs
   -------
   nu                    True anomaly

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Children:

Common: Graphics/Plot2D
Math: Analysis/SHarm

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