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% u v w phi theta psi x y z p q r
% 1 2 3 4 5 6 7 8 9 10 11 12
X_Guess = [60 0 0 0 0 0 0 0 0 0 0 0]';
% e a r thrust
% 1 2 3 4
U_guess = [0 0 0 1000]';
% V alpha beta phi theta psi x y z p q r gamma
% 1 2 3 4 5 6 7 8 9 10 11 12 13
Y_guess = [60 0 0 0 0 0 0 0 0 0 0 0 0]';
Dx_guess = [0 0 0 0 0 0 0 0 0 0 0 0]';
Ix = [2 4 6 10 11 12]';
Iu = [2 3]';
Iy = [1 3 4 6 10 11 12 13]';
Idx = [1 2 3 4 5 6 8 9 10 11 12]';
[x1,u1,y1,dx1] = trim('Cessna_6DOF_trim',X_Guess,U_guess,Y_guess,Ix,Iu,Iy,Dx_guess,Idx);
display(x1)
display(y1)
display(u1)
display(dx1)
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