%
% Medium-sized aircraft
%

A=[-0.154    0.004    0.178    0.075 ;
   -1.25     -2.85      0      1.43  ;
      0        1        0        0   ;
    0.568    -0.277     0     -0.284 ]

B=[ 0.075;
   -0.727;
      0  ;
   -2.05 ]