RHSLunarOrbit:

Path: Missions/LunarMission

% Right hand side for a lunar mission simulation with only orbit dynamics.

 This function implements only orbit dynamics. The Moon gravity model can have
 spherical harmonics. Get the default data structure by typing:

   d = RHSLunarOrbit

 Set up the state name output by typing:

   RHSLunarOrbit( x );

--------------------------------------------------------------------------
   Form:
           d = RHSLunarOrbit            % data structure
               RHSLunarOrbit( x );      % initialize persistent variables
   [xDot, p] = RHSLunarOrbit( x, t, d )
--------------------------------------------------------------------------

   ------
   Inputs
   ------
   x     (:,1)   [rECI;vECI;m]
   t     (1,1)   Time
   d     (.)     Data structure

   -------
   Outputs
   -------
   xDot  (:,1)   dx/dt
   p     (.)     Data structure with internally computed variables

--------------------------------------------------------------------------

Children:

SC: Ephem/MoonRot
Common: Time/DTSToDTA
Common: Time/Date2JD
Math: Linear/Mag

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