Research Article
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 |
|
|