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