Path: Orbit/RHSOrbit

% Right hand side for a heliocentric system with a thruster.

   Uses the ephemerides from Planets and SolarSysState to compute
   the planet locations in the heliocentric frame.

   Since version 2014.1
	 [xDot, g] = RHSHelioWithPlanets( x, t, d )

   x       (7,1)   State in the heliocentric frame [r;v;m]
   t       (1,1)   Time since jD0, sec
   d       (1,1)   Data structure
                   .mDry   (1,1) Dry mass (kg)
                   .thrust (3,1) Heliocentric thrust vector (N)
                   .uE     (1,1) Exhaust velocity (m/s)
                   .p      (1,1) Planet data structure
                   .jD0    (1,1) Julian date at the start of the
   xH      (7,1)   State in the heliocentric frame
   g       (1,1)   Output data structure
                   .accelSun     (3,1) Acceleration due to the sun
                   .accelThrust  (3,1) Acceleration due to the engine
                   .accelPlanet	(3,:) Acceleration due to planets

   See also APlanet


Orbit: Interplanetary/SolarSysState
Orbit: OrbitMechanics/APlanet
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
Math: Linear/Mag

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