2) MATLAB - Write a script to calculate the moment of inertia of the following spacecraft about its center of mass (combined spacecraft and solar panel). Assume the spacecraft body has a density of 1.5 g/cm? and the solar panel has a density of 2.7 g/cm. 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. 45 deg 1.5 m 1.2 m 1.0 m 2.5 m 1.0 m 2) MATLAB - Write a script to calculate the moment of inertia of the following spacecraft about its center of mass (combined spacecraft and solar panel). Assume the spacecraft body has a density of 1.5 g/cm and the solar panel has a density of 2.7 g/cm. 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. 45 deg 1.5 m CM 1.2 m 1.0 m 2.5 m 1.0 m 2) MATLAB - Write a script to calculate the moment of inertia of the following spacecraft about its center of mass (combined spacecraft and solar panel). Assume the spacecraft body has a density of 1.5 g/cm? and the solar panel has a density of 2.7 g/cm. 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. 45 deg 1.5 m 1.2 m 1.0 m 2.5 m 1.0 m 2) MATLAB - Write a script to calculate the moment of inertia of the following spacecraft about its center of mass (combined spacecraft and solar panel). Assume the spacecraft body has a density of 1.5 g/cm and the solar panel has a density of 2.7 g/cm. 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. 45 deg 1.5 m CM 1.2 m 1.0 m 2.5 m 1.0 m