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