Given assembeled mass, stiffness matrices and damping matrices, external load vector of n degree's of freedom, response of the system to the external load is calculated using Wilson tita step-by-step integration method. Time step, tita value can be changed accordingly to the problem.
KSSV (2021). Wilson tita Time Integration Method (https://www.mathworks.com/matlabcentral/fileexchange/32182-wilson-tita-time-integration-method), MATLAB Central File Exchange. Retrieved .
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