FEarthMoon:

Path: Orbit/RHSOrbit

% Gravity acceleration in the earth moon system
--------------------------------------------------------------------------
   Form:
   xDot = FEarthMoon( x, t, jD, muMoon, muEarth )
--------------------------------------------------------------------------

   ------
   Inputs
   ------
   x           (6,1)   [r;v]
   t           (1,1)   Time
   jD          (1,1)   Julian date
   muMoon      (1,1)   Gravitational parameter for the moon
   muEarth     (1,1)   Gravitational parameter for the earth

   -------
   Outputs
   -------
   xDot        (6,1)   State derivative

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

Children:

Math: Linear/Mag
Orbit: OrbitMechanics/APlanet
SC: Ephem/MoonV1

Back to the Orbit Module page