Adaptive Neural Network Sliding Mode Control for Quad Tilt Rotor Aircraft

Table 1

Parameters for experiment.

Parameter	Value
Mass for QTRA (kg)	6.25
(kg⋅m^2)	4.568
(kg⋅m^2)	3.109
(kg⋅m^2)	2.796
(kg⋅m^2)	0.028