RCAIDE.Library.Methods.Mass_Properties.Moment_of_Inertia.compute_vehicle_moment_of_inertia

compute_vehicle_moment_of_inertia

compute_vehicle_moment_of_inertia(vehicle, moment_of_inertia_df, overwrite_moment_of_intertia=True, segment=None, verbose=True)

sums the moments of inertia of each component in the aircraft. Components summed: fuselages, wings (main, horizontal, tail + others), turbofan engines, batteries, motors, batteries, fuel tanks

Assumptions: - All other components than those listed are insignificant

Source:

Inputs: - vehicle - Center of gravity

Outputs: - Total aircraft moment of inertia tensor

Properties Used: N/A