PropagateCRTBPToPeriapse:

Path: Orbit/ThreeBody

% Propagate the CRTBP initial state to the next perigee 

   Since version 9.
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   Form:
   [yF, tF] = PropagateCRTBPToPeriapse(y,t0,tF,mu);
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   ------
   Inputs
   ------
   y              (6,1)    current state vector [r;v] (coordinates are
                           centered at the secondary body)
   t0             (1)      initial time
   tF             (1)      upper bound on final time
   mu             (1)      CRTBP mass ratio

   -------
   Outputs
   -------
   yF             (6,1) 	State at the periapse
   tF             (1)      Time at the periapse
  
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Children:

Orbit: ThreeBody/PropagateCRTBP

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