Path: Orbit/LowEnergyManeuver

% Compute a periodic orbit for a LET transfer.  
 The orbit has nearest periapsis at r1. Loads a mat-file for the specified
 family which must be in the paty.
   [d] = LETGuess( p1, mu, family );

   mu             (1,1)  Gravity ratio of the CRTBP
   p1             (1,1)  Nearest periapse radius
   family         (1,:)  Family name from Markellos catalog
                           - 'f16'
                           - 'f16p'

   d              (:)  Data structure with inforamation about the orbit



AC: ACData/ACTConstants
Orbit: LowEnergyManeuver/CRTBPJacobiConstant
Orbit: LowEnergyManeuver/CheckForOptimizationToolbox
Orbit: LowEnergyManeuver/PeriodicOrbitFromGuess
Orbit: LowEnergyManeuver/PropagateCRTBP
Orbit: LowEnergyManeuver/RHSCRTBP
Orbit: LowEnergyManeuver/V0FromJacobiConstant
Orbit: LowEnergyManeuverData/f16Ref
Orbit: LowEnergyManeuverData/f16pRef
SC: SCData/sCTConstants
Common: CommonData/Constants
Common: CommonData/SwooshWatermark
Common: CommonData/xSplashSmall
Common: Database/Constant
Common: General/CellToMat
Common: General/DeleteCell
Common: General/MatToCell
Common: General/Watermark
Common: Graphics/NewFig
Common: Graphics/Plot2D
Common: Graphics/PltStyle

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