Path: Orbit/OrbitCoord

% Transform Sun-Earth-Moon rotating (SEMR) state to the heliocentric frame.  
 The SEMR coordinate frame is +x pointing at the earth along
 the sun-earth line. +z normal to the sun-earth plane
 and +y completing the set. 

 Type TransformSEMRToHelio for a demo
   [rHelio,vHelio,mRot] = TransformSEMRToHelio( jD, rSEMR, vSEMR )

   jD            (1,:)       Julian date (days)
   rSEMR         (3,:)       Position vector in SEMR frame          
   vSEMR         (3,:)       Velocity vector in SEMR frame          

   rHelio          (3,:)       Position vector in heliocentric frame
   vHelio          (3,:)       Velocity vector in heliocentric frame
   mRot            (3,3)       Rotation matrix

  See also  TransformSEMRToECI and SunV2


AC: ACData/ACTConstants
Orbit: OrbitCoord/TransformECIToSEMR
Orbit: OrbitCoord/TransformSEMRToECI
SC: BasicOrbit/RVFromKepler
SC: Ephem/CEcl2Eq
SC: Ephem/SunV2
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/Plot3D
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/Mag
Math: Linear/Unit
Math: Trigonometry/CosD

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