CRTBPJacobiConstant:

Path: Orbit/LowEnergyManeuver

% Calculate from Jacobi constant from a scaled state vector
 The default three-body problem is the Earth, Moon, and sun.
 Type CRTBPJacobiConstant for a demo with two identical vectors.
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   Form:
   j = CRTBPJacobiConstant(y,mu)
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   ------
   Inputs
   ------
   y   (6,n)	State vector in scaled coordinates [r;v]
   mu	(1,1)	CRTBP mass parameter

   -------
   Outputs
   -------
   j   (n,1)	Jacobi constant
  
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Children:

AC: ACData/ACTConstants
Orbit: LowEnergyManeuverData/f16Ref
SC: SCData/sCTConstants
Common: CommonData/Constants
Common: CommonData/xSplashSmall
Common: Database/Constant
Common: General/DeleteCell

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