Path: Orbit/LowEnergyManeuver

% Calculate the nominal transfer time for a low energy transfer
 The names of the moon and planet must be available in the Constant database.
 Type LETPhasing for a demo.

   [det,orbits] = LETPhasing(x0,desiredPhasing,moon,planet,et,jDate)

   x0            	(1,1) Initial guess for a transfer time
   desiredPhasing	(1,1) Angle of the moon at the final time in the
                         Sun/Planet rotating coordinate system
   moon           	(1,:) String name of moon
   planet         	(1,:) String name of planet
   et            	(1,1) Seconds after the epoch jDate at which the
                         transfer initiates
   jDate           (1,1) Julian date
   det             (1,1) Estimated transfer time
   orbits         	(1,1) Number of lunar orbits during transfer



AC: ACData/ACTConstants
Orbit: LowEnergyManeuver/J20002RotPuls
SC: BasicOrbit/E2M
SC: BasicOrbit/Nu2E
SC: BasicOrbit/Nu2M
SC: BasicOrbit/RV2El
SC: Ephem/CEcl2Eq
SC: Ephem/InterpolateState
SC: Ephem/PlanetPosJPL
SC: Ephem/PlanetPositionEMBarycenter
SC: SCData/bin2000
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
Common: Time/DTSToDTA
Common: Time/Date2JD
Common: Time/JD2000
Math: Linear/Cross
Math: Linear/DupVect
Math: Linear/Mag
Math: Linear/Unit

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