Path: Orbit/RHSOrbit

% Computes the right hand side for a gravity model.
 Allows for any spherical harmonic model to be passed in as a data structure.
 Uses the highest fidelity Earth ephemeris function.
   xDot = RHSGeoHarm( x, t, d )

   x           (6,1)    Position vector [rECI (km); vECI (km)];
   t           (1,1)    Time since start Julian Date (s) 
   d            (.)     Gravity model data structure 
                        .nN	 (1,1)	Highest zonal harmonic (m = 0) 
                        .nM    (1,1)	Highest sectorial and tesseral harmonic 
                        .s     (:,:)	S terms
                        .c     (:,:)	C terms
                        .j     (1,:)	m = 0 terms
                        .mu    (1,1)	Spherical gravitational potential
                        .a     (1,1)	Planet radius
                        .jD0	  (1,1)	Start Julian Date    
                        .isNormalized (1) Coefficient are normalized, or not

   xDot        (6,1)   [rDot;vDot]

 See also: TruEarth, AGravityC


Orbit: GravityModels/LoadGEM
Orbit: GravityModels/NormalizationMatrix
Orbit: OrbitMechanics/AGravityC
SC: Ephem/EOfE
SC: Ephem/EarthNut
SC: Ephem/EarthPre
SC: Ephem/EarthRot
SC: Ephem/GMSTime
SC: Ephem/MSidDay
SC: Ephem/NutDelta
SC: Ephem/ObOfE
SC: Ephem/TruEarth
Common: CommonData/SwooshWatermark
Common: General/CellToMat
Common: General/DeBlankLT
Common: General/DispWithTitle
Common: General/MatToCell
Common: General/Watermark
Common: Graphics/Mesh2
Common: Graphics/NewFig
Common: Graphics/Plot2D
Common: Graphics/PltStyle
Common: Graphics/XLabelS
Common: Graphics/YLabelS
Common: Graphics/ZLabelS
Common: Time/DTSToDTA
Common: Time/Date2JD
Common: Time/JD2000
Common: Time/JD2T
Common: Time/JDToMidnight
Math: Linear/DupVect
Math: Linear/Factorl
Math: MathUtils/R2P5
Math: Trigonometry/CosD
Math: Trigonometry/SinD

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