Research Article
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 |
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