Use LU decomposition to determine the matrix inverse for the following system. Do not use a pivoting strategy, and check your results by verifying that
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EBK NUMERICAL METHODS FOR ENGINEERS
- Determinant of 2 x 2 Matrices. Solve for the determinant of the following matrices: -3 1. A = 6. 4 2. В %3D 9. -3 13 3. C = 1 10 4. D = 3 11 x? – 3y -3x2 -x + 2y2 x²y 5. E =arrow_forwarduse B=00arrow_forwardb) By using Doolittle's or Cholesky Decomposition method X1 + x2 + x3 = 1 4x1 + 3x2 – x3 = 6 3x1 + 5x2 + 3x3 = 4arrow_forward
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- アN 0. 2. B=2 Matrix ) Find all the eigen values. ) Calculate the eigenvector correspon ding to the Caleulare largest eigenvalue.arrow_forwardtake x=2 use graph harrow_forwardI am trying to find a Direction Cosine Matrix (DCM) for the Euler angle body 1-2-3 sequence. I tried making my own function and using the MATLAB function, but the result is matrices that are not equal to each other. But, if I were to use the 'ZYX' sequence, I would get a matrix that is equal to the transpose of the matrix produced by my function.I mean that transpose(EA123toDCM) = E123toDCM if I changed the sequence to 'ZYX'. I never got two equal matrices. Can you fix my code so I would get two equal DCM matrices for the body 1-2-3 sequence? Also, for the E123toDCM line, I am using the sequence 'XYZ'. Is that correct or should it be 'ZYX'? I know that that for a DCM of sequence 1-2-3 = R3(theta1)*R2(theta2)*R1(theta3). Is ZYX sequence the same as a 1-2-3 sequence? EA = [pi/3; -pi/4; -pi/6];EA123toDCM = EA123DCM(EA) E123toDCM = angle2dcm(EA(1,1), EA(2,1), EA(3,1), 'XYZ') function [R] = EA123DCM(EA) theta1 = EA(1,1); theta2 = EA(2,1); theta3 = EA(3,1); R1 =…arrow_forward
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