Calculate the principal inertia tensor, Jp, and the principal rotation matrix, Cp, for a spacecraft with the following inertia tensor: J=kg.m2 Use the result to find the angular velocity in the...

Calculate the principal inertia tensor, Jp, and the principal rotation matrix, Cp, for a spacecraft with the following inertia tensor: J=kg.m²

Use the result to find the angular velocity in the principal frame if the angular velocity in the current body frame is ω = (0.15, −0.25, −0.8)^T
rad/s.