This is a space mechanics and matlab coding problem.

Find the numerical solution to the torque-free attitude dynamics EOM by using MATLAB. (EOM means Euler's rotational EOM. USE A=B with omega_z=constant. i.e., Axi- symmetric spinning body. You are supposed to find omega_x and omega_y) You need to present the solution as a graph (time vs value) since the answers are not a function. Submit the codes and graphs in a pdf file. Find the numerical solution to the torque-free attitude dynamics EOM by using MATLAB. (EOM means Euler's rotational EOM. USE A=B with omega_z=constant. i.e., Axi- symmetric spinning body. You are supposed to find omega_x and omega_y) You need to present the solution as a graph (time vs value) since the answers are not a function. Submit the codes and graphs in a pdf file