EulRate:

Path: AC/ACCoord

% Euler rates.
--------------------------------------------------------------------------
   Form:
   eDot = EulRate( e, w )
--------------------------------------------------------------------------

   ------
   Inputs
   ------
   e           (3,1) Euler angles [phi;theta;psi]
   w           (3,1) Angular rates wrt NED [p;q;r]

   -------
   Outputs
   -------
   eDot        (3,1) Euler rates d[phi;theta;psi]/dt

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

Back to the AC Module page