EulNED:

Path: AC/ACCoord

% Euler angles given ECI information.
   Since version 2 (ACT)
--------------------------------------------------------------------------
   Form:
   e = EulNED( r, qECIToB, e )
--------------------------------------------------------------------------

   ------
   Inputs
   ------
   r           (3,1) ECI Position vector
   qECIToB     (4,1) Quaternion from ECI to B
   e           (3,1) Euler angles [phi;theta;psi]

   -------
   Outputs
   -------
   e           (3,1) Euler angles [phi;theta;psi]

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   Reference: Stevens, B.L., Lewis, F.L. , Aircraft Control and Simulation,
              John Wiley & Sons, 1992, p. 38.
--------------------------------------------------------------------------

Children:

AC: ACCoord/ECIToNED
Common: Quaternion/Q2Eul
Common: Quaternion/QMult
Common: Quaternion/QPose

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