PropagateCRTBPToXAxis:

Path: Orbit/LowEnergyManeuver

% Propagate the  CRTBP equations of motion for arbitrary mu 
 Finds the state when the trajectory hits the x-axis.
 
 Type PropagateCRTBPToXAxis for a demo
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   Form:
   [tF, yF] = PropagateCRTBPToXAxis(y,t0,tol,mu);
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   ------
   Inputs
   ------
   y   (6,1) Current state vector [r;v]
   t0	(1,1) Initial time
   tol	(1,1) Convergence tolerance
   mu	(1,1)	CRTBP mass ratio

   -------
   Outputs
   -------
   tF	(1,1)	Time at the intersection with the x-axis
   yF	(6,1)	State at the intersection with the x-axis
  
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Children:

Orbit: LowEnergyManeuver/PropagateCRTBP
Orbit: LowEnergyManeuverData/f16pRef
Common: Graphics/NewFig
Math: Linear/Mag

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