Path: Orbit/OrbitCoord

% Generates an array of true anomalies. 

   [nu, dT, t] = TrueAnomalySpacing( e, nu0, n, duration, nS, eTol )

   e           (1,1)   Eccentricity
   nu0         (1,1)   Initial true anomaly (rad)
   n           (1,1)   Mean orbit rate (rad/s)
   duration    (1,1)   Duration of array (sec)
   nS          (1,1)   Total number of samples
   eTol        (1,1)   Tolerance on e (circular orbit)

   nu          (1,:)	True anomalies
   dT          (1,:)	Time steps
   t           (1,:+1)	Time vector



SC: BasicOrbit/E2M
SC: BasicOrbit/E2Nu
SC: BasicOrbit/M2E
SC: BasicOrbit/M2EApp
SC: BasicOrbit/M2EEl
SC: BasicOrbit/M2EHy
SC: BasicOrbit/M2Nu
SC: BasicOrbit/M2NuAbs
SC: BasicOrbit/M2NuPb
SC: BasicOrbit/Nu2E
SC: BasicOrbit/Nu2M
Common: CommonData/SwooshWatermark
Common: General/CellToMat
Common: General/MatToCell
Common: General/Watermark
Common: Graphics/NewFig
Common: Graphics/Plot2D
Common: Graphics/PltStyle
Math: Linear/DupVect
Math: Trigonometry/UnwrapPhase

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