Research Article

Robust Data-Driven Fault Detection: An Application to Aircraft Air Data Sensors

Table 4

ADS fault cases adopted in this paper.

CaseSensorFault typeMagnitude

5Sideslip angleExtra noise5°~10°
4Sideslip angleDrift±5°~10°
3AOAExtra noise5°~10°
2AOADrift±5°~10°
1AirspeedDrift-50%~100%
0Clean measurement with noises and disturbances, no fault

Noise standard deviation and drift values defined in this column.