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

Table 2

The maximum deviation of variables during time-varying faults.

The error of variables	PID	ADRC	RBF-ADRC
Angle of attack error (deg)	0.018	0.018	0.00825
Path angle error (deg)	0.0057	0.0029	0.00239
Pitch angle error (deg)	0.129	0.018	0.006
Pitch rate error (deg)	0.0158	0.0134	0.015
Velocity error (m/s)	1.48	1.26	0.94
Tracking error (m)	0.278	0.125	0.051