Research Article
Air Data Sensor Fault Detection with an Augmented Floating Limiter
(a) Performance for TAS: robustness against false alarms |
| Airspeed | Flight duration (min) | False alarms (number of samples) | Maximum stay out of thresholds (sec) |
| Flight-1 | 17 | 7 | 0.4 | Flight-2 | 17.3 | 0 | 0 | Flight-3 | 18 | 0 | 0 | Flight-4 | 28.3 | 0 | 0 | Flight-5 | 30.8 | 22 | 0.6 |
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(b) Performance for : robustness against false alarms |
| Angle of attack | Flight duration (min) | False alarms (number of samples) | Maximum stay out of thresholds (sec) |
| Flight-1 | 17 | 35 | 0.4 | Flight-2 | 17.3 | 8 | 0.3 | Flight-3 | 18 | 0 | 0 | Flight-4 | 20.3 | 34 | 0.6 | Flight-5 | 28.3 | 0 | 0 | Flight-6 | 30.8 | 56 | 0.7 |
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(c) Performance for : robustness against false alarms |
| Angle of sideslip | Flight duration (min) | False alarms (number of samples) | Maximum stay out of thresholds (sec) |
| Flight-1 | 17.3 | 0 | 0 | Flight-2 | 18 | 0 | 0 | Flight-3 | 20.3 | 40 | 1.5 | Flight-4 | 19.9 | 42 | 1.6 | Flight-5 | 30.8 | 120 | 2.2 |
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