RV2ElDPT:

Path: Plotting/Derivation Functions

% Transform ECI position and velocity into orbital elements.
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   Form:
   out = RV2ElDPT( varargin )
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   ------
   Inputs
   ------
   varargin         (:)   Variable number of inputs, raw simulation data.

   -------
   Outputs
   -------
   out             (1,:)  Derived output data.

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

Children:

SC: BasicOrbit/E2M
SC: BasicOrbit/Nu2E
SC: BasicOrbit/Nu2M
SC: BasicOrbit/RV2El
Common: CommonData/SwooshWatermark
Common: General/CellToMat
Common: General/MatToCell
Common: General/Watermark
Common: Graphics/NewFig
Common: Graphics/Plot2D
Common: Graphics/PltStyle
Math: Linear/Cross
Math: Linear/DupVect
Math: Linear/Mag

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