AE2VR:

Path: Orbit/OrbitCoord

% Computes v and r given a, e and nu.
   Also gives the time for each step.
--------------------------------------------------------------------------
   Form:
   [v, r, t] = AE2VR( a, e, nu, mu )
--------------------------------------------------------------------------

   ------
   Inputs
   ------
   a           (1,1)    Semi major axis
   e           (1,1)    Eccentricity
   nu          (1,n)    True anomaly (rad)
   mu          (1,1)    Gravitational parameter (default = 3.98600436e5)

   -------
   Outputs
   -------
   v           (1,n)    Velocity
   r           (1,n)    Radius
   t           (1,n)    Time

--------------------------------------------------------------------------

Children:

Orbit: OrbitCoord/RPRA2AE
SC: BasicOrbit/E2M
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

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