If the body of the helicopter is pitching forward at a constant rate Ωbody=⎣⎡0ωpitch0⎦⎤ and has constant main-rotor rotational speed, what is the contribution to the moment of inertia about the pitch axis? A) 0 B) ωₚᵢₜ꜀ₕ C) ωₚᵢₜ꜀ₕ² D) 1/2ωₚᵢₜ꜀ₕ² E) None of the above
