M2Nu:

Path: Orbit/OrbitMechanics

% Computes the true anomaly from the mean anomaly.

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   Form:
   nu  = M2Nu( e, M, tol, nMax )
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   ------
   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)

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Children:

Orbit: OrbitMechanics/E2Nu
Orbit: OrbitMechanics/M2E
Orbit: OrbitMechanics/M2NuPb
Common: Graphics/Plot2D

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