RCAIDE.Library.Methods.Mass_Properties.Moment_of_Inertia.compute_cabin_moment_of_inertia

compute_cabin_moment_of_inertia

compute_cabin_moment_of_inertia(cabin, fuselage, center_of_gravity=array([[0, 0, 0]]))

Computes the moment of inertia tensor for the cabin.

Parameters:

center_of_gravity (list, optional) – Reference point coordinates for moment calculation, defaults to [[0, 0, 0]]

Returns:

I – 3x3 moment of inertia tensor in kg*m^2

Return type:

ndarray

See also

RCAIDE.Library.Methods.weights.vehicle.moments_of_inertia.compute_fuselage_moment_of_inertia

Implementation of the moment of inertia calculation