FFEccTargetTrueAnom:

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   Compute the future true anomaly (unwrapped) at the specified number of orbits 
   after the initial true anomaly. 

   Since version 7.
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   ------
   Inputs
   ------
   e             (1)  Eccentricity
   nu0           (1)  Initial true anomaly  [rad]
   nOrb         (1,:) Time vector from initial true anomay [orbit periods]

   -------
   Outputs
   -------
   nuF          (1,:)  Vector of final true anomalies
   
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Children:

Math: Trigonometry/WrapPhase
OrbitMiniToolbox: Support/M2Nu
SC: BasicOrbit/Nu2M