EKF-Based Actuator Fault Detection and Diagnosis Method for Tilt-Rotor Unmanned Aerial Vehicles

Table 1

Physical parameters of the tilt-rotor UAV.

Parameters	Value
Weight	65 kg
Wing area	4.01 m^2
Mean aerodynamic wing chord	1.27 m
Wing span	3.15 m
Moment of inertia	53.31 kg m^2
Moment of inertia	18.38 kg m^2
Moment of inertia	69.47 kg m^2