truss system problem solve for matlab
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a=cos(pi/6); 
b=cos(pi/3); 
%  Fab Fag Fbc Fbg Fcd Fcf Fcg Fde Fdf Ffe Fgf Ax Ay Ey
T=[ b   1   0   0   0   0   0   0   0   0   0   1  0  0 ;% Ax
    a   0   0   0   0   0   0   0   0   0   0   0  1  0 ;% Ay
   -b   0   1   b   0   0   0   0   0   0   0   0  0  0 ;% Bx
   -a   0   0   a   0   0   0   0   0   0   0   0  0  0 ;% By
    0   0  -1   0   1   b   b   0   0   0   0   0  0  0 ;% Cx
    0   0   0   0   0   a   a   0   0   0   0   0  0  0 ;% Cy
    0   0   0   0  -1   0   0   b   b   0   0   0  0  0 ;% Dx
    0   0   0   0   0   0   0   a   a   0   0   0  0  0 ;% Dy
    0   0   0   0   0   0   0  -b   0  -1   0   0  0  0 ;% Ex
    0   0   0   0   0   0   0  -a   0   0   0   0  0  1 ;% Ey
    0   0   0   0   0  -b   0   0  -b   1  -1   0  0  0 ;% Fx
    0   0   0   0   0  -a   0   0  -a   0   0   0  0  0 ;% Fy
    0  -1   0  -b   0   0  -b   0   0   0   1   0  0  0 ;% Gx
    0   0   0  -a   0   0  -a   0   0   0   0   0  0  0 ];% Gy
F=[ 0; 0;0;0;0; 0;0; 0;0; 0;0;-8;0;-6 ]; % Applied forces, as shown on the truss
Y=inv(T);
(Y)*(-F)



3 Commenti
  ibrahim Çevikgil
 il 14 Gen 2023
				Bilal merhaba aktif olarak burdaysan dönüş sağlayabilir misin bu yoruma sorumu özel olarak iletiyim. 
Risposte (1)
  Manikanta Aditya
      
 il 20 Giu 2022
        Hi Bilal, 
I understand that you are trying to solve truss system problems in MATLAB. I found a code for reference, which returns the global stiffness matrix of a given truss system. So, you could refer to the link below to get some understanding of the solution.  
For reference: 
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