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   Generate a time vector evenly spaced over true anomaly 
  (for an eccentric orbit)
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   Form:
   [t,M,nu] = GenerateTimeVector(d,tF,nPts)
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   ------
   Inputs
   ------
   d          (:)    Collision data structure
   tF        (1,1)   Final propagated time
   nPts      (1,1)   Number of discretization points per orbit

   -------
   Outputs
   -------
   t         (1,n)   Time vector
   M         (1,n)   Mean anomaly vector
   nu        (1,n)   True anomaly vector

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