Path: Orbit/RHSOrbit

% High fidelity orbit model right-hand-side. 
   Includes higher harmonics of the earth's gravitational field and sun and 
   moon accelerations as options.
   The drag option = drag coefficient * area / mass where the area is in m^2
   The sun option = area / mass
   The moon option is 0 or 1
   See also AGravity, APlanet, AtmDens2, SolarF, and FOrb.

   Since version 1.
   xDot = FOrbHF( x, t, options, jD, aExt, mu, s, c, j, a )
   xDot = FOrbHF( t, x, options, jD, aExt, mu, s, c, j, a )  (for ode113)

   x             (6,1)    The state vector [x;y;z;dx/dt;dy/dt;dz/dt]
   t                      Time
   options         (5)    [Highest zonal harmonic,Highest tesseral harmonic,
   jD                     Julian date
   aExt            (3)    External acceleration vector [x;y;z] ECI
   mu                     Spherical gravitational potential
   s           (36,36)    S terms
   c           (36,36)    C terms
   j              (36)    m = 0 terms
   a                      Earth radius

   xDot         (6,1)     The derivative of the state state vector



AerospaceUtils: AtmosphericCalculations/AtmDens2
AerospaceUtils: AtmosphericCalculations/AtmJ70
AerospaceUtils: Coord/ECIToEF
Common: Time/JD2T
Math: Linear/Cross
Math: Linear/Mag
Math: Linear/Unit
Orbit: OrbitMechanics/AGravity
Orbit: OrbitMechanics/APlanet
SC: BasicOrbit/FOrbCart
SC: Disturbances/SolarF
SC: Ephem/Eclipse
SC: Ephem/MoonV1
SC: Ephem/SunV1

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