Can anyone please help me out with this problem!!

Using CLT, the ABD matrix was formulated to relate the laminate loads to its midplane deformations. Relations were developed to relate midplane deformation to laminate strain and laminate strains to laminate stresses. A stepwise algorithmic procedure is outlined below. The algorithm is to be used to perform stress analysis for any given laminate. You are to use the procedure and develop a MATLAB code to be used to analyze any laminate Documentation of vour code must be detailed and your printed data should have proper and meaningful headings. 1. Define your analysis parameters. 2. Read in and print the laminate number of layers. 3. Read in and print the thickness, orientation and the engineering properties of each layer. 4. Compute and print the Qj matrix for each layer. 5. Compute and print the Qi-bar matrix for each layer. 6. Compute and print the zk values. 7. Compute and print the components of the A, B, and D matrices. Using CLT, the ABD matrix was formulated to relate the laminate loads to its midplane deformations. Relations were developed to relate midplane deformation to laminate strain and laminate strains to laminate stresses. A stepwise algorithmic procedure is outlined below. The algorithm is to be used to perform stress analysis for any given laminate. You are to use the procedure and develop a MATLAB code to be used to analyze any laminate Documentation of vour code must be detailed and your printed data should have proper and meaningful headings. 1. Define your analysis parameters. 2. Read in and print the laminate number of layers. 3. Read in and print the thickness, orientation and the engineering properties of each layer. 4. Compute and print the Qj matrix for each layer. 5. Compute and print the Qi-bar matrix for each layer. 6. Compute and print the zk values. 7. Compute and print the components of the A, B, and D matrices