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% The FDC toolbox - Examples of using FDC models and tools.
% =========================================================
% The directory EXAMPLES contains demo-files for the FDC toolbox.
% The following files are contained in this directory:
%
% OLOOP1.MDL Simulink system for evaluating open-loop responses of the
% 'Beaver' aircraft to block or ramp-shaped control inputs to
% the elevator, rudder, ailerons, flaps, manifold pressure,
% and/or engine RPM.
%
% OLOOP1T.MDL 'Tutorial', describing the construction of OLOOP1. This system
% explains the meaning of the different blocks from OLOOP1.
%
% OLOOP2.MDL Simulink system for evaluating open-loop responses of the
% 'Beaver' aircraft to atmospheric turbulence.
%
% OLOOP2T.MDL 'Tutorial', describing the construction of OLOOP2. This system
% explains the meaning of the different blocks from OLOOP1.
%
% OLOOP3.MDL Simulink system for evaluating open-loop responses of the
% 'Beaver' aircraft to control inputs, using a linearized version
% of the aircraft model (linear state-space matrices determined
% by applying the linearization program ACLIN to the non-linear
% aircraft model BEAVER.MDL from the directory AIRCRAFT).
%
% OLOOP3T.MDL 'Tutorial', describing the construction of OLOOP3. This system
% explains the meaning of the different blocks from OLOOP3.
%
% TRIMDEMO.M Demonstration of the steady-state trim option, applied to the
% S-function BEAVER. This demo computes steady-state values for
% the elevator deflection as a function of the true airspeed
% and puts the results in a figure. The source-code of this
% demo has been copied largely from the routine ACTRIM.M, con-
% tained in the directory TOOLS.
%-------------------------------------------------
% The FDC toolbox. Copyright Marc Rauw, 1994-2000.
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