Path: Orbit/Interplanetary

% Initialize a heliocentric orbit from a planet centered orbit.

   xP is in the ECI planet centered frame.

   Type HelioFromPlanetInit for a demo of an equatorial 7000 km circular
   earth orbit.

   This only works with the planets (including Pluto).

   Since version 2014.1
   xH = HelioFromPlanetInit( planet, xP, jD )

   name    (1,1)   Planet name
   xP      (6,1)   State in the planet centered ECI frame
   jD      (1,1)   Julian date      

   xH      (6,1)   State in the heliocentric frame



AC: ACData/ACTConstants
SC: BasicOrbit/E2Nu
SC: BasicOrbit/M2E
SC: BasicOrbit/M2EApp
SC: BasicOrbit/M2EEl
SC: BasicOrbit/M2EHy
SC: BasicOrbit/M2Nu
SC: BasicOrbit/M2NuPb
SC: Ephem/CEcl2Eq
SC: Ephem/Planets
SC: Ephem/SolarSys
SC: SCData/sCTConstants
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/NewFig
Common: Graphics/Plot2D
Common: Graphics/PltStyle
Common: Graphics/TextS
Common: Graphics/XLabelS
Common: Graphics/YLabelS
Common: Time/DTSToDTA
Common: Time/Date2JD
Common: Time/JD2T
Math: Linear/DupVect

Back to the Orbit Module page