Fault-Tolerant Control for Carrier-Based Aircraft Automatic Landing Subject to Multiple Disturbances and Actuator Faults

Table 1

The maximum deviation of variables at constant faults.

The error of variables	PID	ADRC	RBF-ADRC
Angle of attack error (deg)	0.0143	0.009	0.0061
Path angle error (deg)	0.0054	0.0032	0.0023
Pitch angle error (deg)	0.01	0.0092	0.0044
Pitch rate error (deg)	0.0094	0.0075	0.008
Velocity error (m/s)	1.25	0.87	0.7
Tracking error (m)	0.224	0.116	0.052