Path: Orbit/Interplanetary

% Find the Julian Date for a straight line trajectory to the target
 Starts at jD0. You specify the [departure target] planets using JPL
 ids, where 1 = Mercury and 9 = Pluto. jD0 may be a Julian day number or date

   [year month day hour minute second]

 Type JDStartTransfer for a demo.
   jDS = JDStartTransfer( jD0, planetPair, transferTime, duration, n )

   jD0           (1,1) Julian date to start computation or date array
   planetPair    (1,2) Planets [departure target]
   transferTime  (1,1) Duration of the transfer (years)
   duration      (1,1) Duration of the study (years)
   n             (1,1) Number of steps

   jDD           (1,1) Departure date



AC: ACData/ACTConstants
Orbit: OrbitCoord/SLR
Orbit: OrbitMechanics/RVOrbGen
SC: BasicOrbit/CP2I
SC: BasicOrbit/E2M
SC: BasicOrbit/E2Nu
SC: BasicOrbit/M2E
SC: BasicOrbit/M2EApp
SC: BasicOrbit/M2EEl
SC: BasicOrbit/M2EHy
SC: BasicOrbit/Nu2E
SC: BasicOrbit/Nu2M
SC: Ephem/CEcl2Eq
SC: Ephem/InterpolateState
SC: Ephem/PlanetPosJPL
SC: SCData/bin2000
SC: SCData/sCTConstants
SC: Visualization/HelioPlot
Common: CommonData/Constants
Common: CommonData/SwooshWatermark
Common: CommonData/xSplashSmall
Common: Database/Constant
Common: General/CellToMat
Common: General/DeBlankLT
Common: General/DeleteCell
Common: General/MatToCell
Common: General/Watermark
Common: Graphics/Axis3D
Common: Graphics/Mesh2
Common: Graphics/NewFig
Common: Graphics/Plot2D
Common: Graphics/PltStyle
Common: Graphics/TimeLabl
Common: Graphics/XLabelS
Common: Graphics/YLabelS
Common: Graphics/ZLabelS
Common: Time/DTSToDTA
Common: Time/Date2JD
Common: Time/JD2000
Math: Linear/DupVect
Math: Linear/Unit

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