📄 kpahrah.m
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function [Ktheta,Kq,Ki_1,Kphi,Kr,dar,drr,Ki_2] = kpahrah(Vref)
%-------------------------------------------------------------
% KPAHRAH.M sets the gain factors for the simulation models
% PAH.M, RAH.M, and PAHRAH.M as a function of the velocity
% of the aircraft (those systems do not contain the complete
% gain-scheduling functions from the complete simulation
% models APILOT1, APILOT2, and APILOT3). The reference
% velocity must be entered as input argument to this func-
% tion. Without input arguments it will be set to 45 m/s.
%-------------------------------------------------------------
% The input argument Vref contains the reference velocity for which the
% gains must be computed. If it is empty, the default velocity of 45 m/s
% will be used instead (mean velocity of 'Beaver' flight envelope).
% ----------------------------------------------------------------------
if nargin == 0
Vref = 45;
end
% Gains for Pitch Attitude Hold mode (no turn-compensation).
% ----------------------------------------------------------
Ktheta = -0.001375*Vref^2 + 0.1575*Vref - 4.8031;
Kq = -0.000475*Vref^2 + 0.0540*Vref - 1.5931;
Ki_1 = 0.5;
% Gains for Roll Attitude Hold mode.
% ----------------------------------
Kphi = 0.000975*Vref^2 - 0.108*Vref + 2.335625;
Kr = -4;
dar = 0.165;
drr = -0.000075*Vref^2 + 0.0095*Vref - 0.4606;
Ki_2 = 0.25;
%---------------------------------------------------------------------------------
% The FDC toolbox. Copyright Marc Rauw, 1994-2000.
% Last revision of this program: October 5, 1997.
%
% Revision history since October 5, 1997:
% =======================================
% October 5, 1997
% - Included input argument Vref and gains as output arguments
% - Removed unnecessary disp commands for better user-interface consistency
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