A vector from the aircraft center of mass to a point on the wing is along the y-direction of the aircraft (body) reference frame and has a magnitude pf 7.5 m. At an instant in time, the orientation of the aircraft is given by ø = 13deg, 0 = 10deg, and p = 108deg. Calculate the z -component of the vector in the Earth frame (in m ).

A vector from the aircraft center of mass to a point on the wing is along the y-direction of the aircraft (body) reference frame and has a magnitude pf 7.5 m. At an instant in time, the orientation of the aircraft is given by ø = 13deg, 0 = 10deg, and p = 108deg. Calculate the z -component of the vector in the Earth frame (in m ).