Path: Orbit/Interplanetary

% Computes planet heliocentric states for a range of dates.

   The data structure is from Planets. 

   Since version 2014.1
   x = SolarSysState( d, jD )

   d   (.)      Data structure
                .iv      (n,2)   Inclination wrt ecliptic plane     (rad)
                .Wv      (n,2)   Longitude of ascending node wrt vernal equinox  (rad)
                .wv      (n,2)   Argument of perhelion      (rad)
                .av      (n,2)   Mean distance (au)
                .ev      (n,2)   Eccentricity
                .Lv      (n,3)   Mean longitude (rad)
                .name    (n,:)   Name of planet
                .jdref   (1,1)   Reference Julian date
                .T       (1,:)   Julian centuries from J2000.0   (centuries)
   jD (1,:)     Julian date

   x  (6,:,:)   [state,date,planet]



SC: BasicOrbit/E2Nu
SC: BasicOrbit/M2E
SC: BasicOrbit/M2EApp
SC: BasicOrbit/M2EEl
SC: BasicOrbit/M2EHy
SC: BasicOrbit/M2Nu
SC: BasicOrbit/M2NuPb
SC: Ephem/Planets
SC: Ephem/SolarSys
Common: CommonData/SwooshWatermark
Common: General/CellToMat
Common: General/DeBlankLT
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

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