RandomOrbit:

Path: Orbit/OrbitMechanics

% Monte-Carlo orbit simulation.

   Type RandomOrbit for a demo with 2008 AE9

   Since version 11.
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   Form:
   [r1S, v1S, rN, vN] = RandomOrbit( el, el1S, t, mu, n )
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   ------
   Inputs
   ------
   elI     (1,6) Elements vector [a,i,W,w,e,M]
   el1S    (1,6) Gaussian noise vector [a,i,W,w,e,M]
   t       (1,1) Times from 0 to ƒ (sec)
   mu      (1,1) Gravitational parameter
   

   -------
   Outputs
   -------
   r1S     (3,1)  Mean position 1 sigma (km)
   v1S     (3,1)  Mean velocity 1 sigma (km)
   rN      (3,1)  Nominal position (km)
   vN      (3,1)  Nominal velocity (km)

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

Children:

Common: Database/Constant
Math: Linear/Mag
Orbit: OrbitMechanics/RVOrbGen

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