Write a MATLAB 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 1.5 /3 and the solar panel has a density of 2.7 g/3. The solar panel has a thickness of 2 cm, is centered on the side of the spacecraft bus, and it has a -45 degree rotation about the y-axis.