OutOfPlane:

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   Computes the delta-v's required for an out-of-plane maneuver.

   Since version 7.
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   ------
   Inputs
   ------
   meas_elem             (1,6)  Reference orbital elements             (Alfriend format) 
                                                                       [a,theta,i,q1,q2,W]
   delta_elem            (:,6)  Error in orbital element differences   (Alfriend format)
   accNom                 (1)   Nominal acceleration                   [km/s/s]
   dTMin                  (1)   Minimum achievable burn duration       [sec]

   -------
   Outputs
   -------
   burnData               (.)  Burn data structure with burn time, 
                                duration, magnitude and direction.
   nBurns                 (1)  Number of burns required
   th1                    (1)  Argument of latitude at which burn is applied
                                (req'd for in-plane delta-v calculations)
   
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Children:

Common: Database/Constant
FormationFlying: Utility/TimeUntilTheta