Question Statement:
The aircraft velocity (m/s) components in body axes are given as [ u, v, w] = [100, 10, 10]. The air
velocity (m/s), angle of attack (deg) and sideslip angle (deg) in that order are
(A) [120, 0.1, 0.1] (B) [100, 0.1, 0.1] (C) [100.995, 0.1, 5.73] (D) [100.995, 5.71, 5.68]