7 An airplane is flying at a velocity of 150 ft/s. At an angle of attack o 12 deg and sideslip of 2 deg, the instantaneous angular velocities ir pitch, roll, and yaw measured by onboard rate gyros are 10 deg/s 5 deg/s, and 10 deg/s, respectively. If the instantaneous values o a and ẞ are 3 deg/s and -5 deg/s, respectively, determine the wind axis angular velocity components Pw, qw, and rw.