A Multibody Model of Tilt-Rotor Aircraft Based on Kane’s Method

Table 1

XV-15 design parameters.

Parameter	Value
(kg)	3991.6
(kg)	1905.1
(m)	0.1448
(m)	-0.9068
(m)	0.4572
(kg·m^2)	48895
(kg·m^2)	55208
(kg·m^2)	96391
(kg·m^2)	10153
(kg·m^2)	2989
(kg·m^2)	10362