If the body of the helicopter is pitching forward at a constant rate Ωbody​=⎣⎡​0ωpitch​0​⎦⎤​ 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) 1/2​ωₚᵢₜ꜀ₕ²​
E) None of the above