Question: 2) MATLAB - Write a script to calculate the moment of inertia matrix of the following spacecraft about its center of mass (combined spacecraft and

2) MATLAB - Write a script to calculate the moment of inertia matrix of the following spacecraft about its center of mass (combined spacecraft and solar panel). Assume the spacecraft body has a density of 1.5g/cm3 and the solar panel has a density of 2.7g/cm3. The solar panel has a thickness of 2cm, is centered on the side of the spacecraft bus, and it has a 45 degree rotation about the y-axis. 3) Given the following moment of inertia matrix. Solve the Eigen problem (by hand) to calculate the principle axis of inertia. J=1500100027001000300 4) MATLAB - write a script to calculate the principle axis of inertia from problem 3. Compare your MATLAB results to your hand solutions from problem 3. Are there any differences? If there are, why might they be different, and are both solutions valid? Hint: Use the built in MATLAB function eig()

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