 state, 4 control, 10 output) 
%
%   x_f16 states:
%       x_f16(1)  = air speed, VT                           (ft/s)
%       x_f16(2)  = angle of attack, alpha                  (rad)
%       x_f16(3)  = angle of sideslip, beta                 (rad)
%       x_f16(4)  = roll angle, phi                         (rad)
%       x_f16(5)  = pitch angle, theta                      (rad)
%       x_f16(6)  = yaw angle, psi                          (rad)
%       x_f16(7)  = roll rate, P                            (rad