RV2Eq:

Path: Orbit/OrbitCoord

% Converts R and V to Equinoctial elements
--------------------------------------------------------------------------
   Form:
   eq = RV2Eq( r, v, mu )
--------------------------------------------------------------------------

   ------
   Inputs
   ------
   r               (3,1) Position vector
   v               (3,1) Velocity vector
   mu                    Gravitational constant

   -------
   Outputs
   -------
   eq                    Elements vector [a,P1,P2,Q1,Q2,l]

--------------------------------------------------------------------------
	  References:	  Bate, R.R., et. al. Fundamentals of Astrodynamics, pp. 70-71.
--------------------------------------------------------------------------

Children:

Orbit: OrbitCoord/El2Eq
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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