AeroD:

Path: AC/Aircraft

% Compute the state space system based on aerodynamic derivatives.
   See DC8.m for an example of the database format.
   The state vector is either:

   'wind':      [vT; alpha; beta; p; q; r; phi; theta; psi]

   or

   'stability': [u; v; w; p; q; r; phi; theta; psi]

   Since version 2 (ACT)
--------------------------------------------------------------------------
   Form:
   [g, gLat, gLon] = AeroD( f, axisSystem )
--------------------------------------------------------------------------

   ------
   Inputs
   ------
   f                     Aircraft data or database for input
   axisSystem            'wind', 'stability'

   -------
   Outputs
   -------
   g                     State space system of type statespace
   gLat                  Lateral dynamics
   gLon                  Longitudinal dynamics

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

Children:

Common: Classes/@statespace/and.m
Common: Classes/@statespace/close.m
Common: Classes/@statespace/connect.m
Common: Classes/@statespace/eig.m
Common: Classes/@statespace/get.m
Common: Classes/@statespace/getabcd.m
Common: Classes/@statespace/getsub.m
Common: Classes/@statespace/isempty.m
Common: Classes/@statespace/mtimes.m
Common: Classes/@statespace/plus.m
Common: Classes/@statespace/series.m
Common: Classes/@statespace/set.m
Common: Classes/@statespace/statespace.m
Common: Control/EigEval
Common: Control/SVPlot
Common: Control/Step

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