MS 132 NASA, Hampton, VA 23681

Initial version A simple constant mass matrix for a 400,000-kg orbiting space station (ISS-like) Rolling moment of inertia about the body X axis Pitching moment of inertia about the body Y axis Yawing moment of inertia about the body Z axis Cross-product of inertia in the body X-Z plane Cross-product of inertia in the body X-Y plane Cross-product of inertia in the body Y-Z plane Total mass of vehicle Longitudinal location of the center of mass relative to the geometric center of the space station, positive if the CM is in front of the center Lateral location of the center of mass relative to the geometric center of the space station, positive if the CM is to the right of the center Vertical location of the center of mass relative to the geometric center of the space station, positive if the CM is below the center