Research Article
Robust Data-Driven Fault Detection: An Application to Aircraft Air Data Sensors
Table 7
Confusion matrix in testing the DNN-opt.
| Aircraft and condition | FD accuracy in cases {0-5} (%) | Aircraft and condition | FD accuracy in cases {0-5} (%) |
| manual LTO | 92.08 | 0.40 | 0.24 | 1.28 | 3.16 | 2.84 | AP cruise | 93.66 | 0 | 0 | 2.46 | 2.16 | 1.72 | 7.24 | 92.43 | 0 | 0 | 0.33 | 0 | 0 | 100 | 0 | 0 | 0 | 0 | 3.54 | 0 | 90.16 | 2.97 | 1.63 | 1.70 | 0.06 | 0 | 96.64 | 0.47 | 1.53 | 1.30 | 2.18 | 0 | 0.07 | 96.70 | 0 | 1.05 | 2.28 | 0 | 0.78 | 95.52 | 0 | 1.42 | 3.27 | 0 | 0 | 0.08 | 95.83 | 0.82 | 3.32 | 0 | 0.14 | 0.34 | 94.98 | 1.22 | 1.71 | 0 | 0.47 | 0.54 | 0.31 | 96.97 | 3.95 | 0 | 0.25 | 0.67 | 0.34 | 94.79 | Aircraft and condition | FD accuracy in cases {0-5} (%) | Aircraft and Condition | FD accuracy in cases {0-5} (%) | manual flight | 90.00 | 0 | 0 | 0 | 2.00 | 8.00 | manual flight | 98.44 | 0 | 0 | 0 | 0.39 | 1.17 | 0 | 100 | 0 | 0 | 0 | 0 | 0 | 100 | 0 | 0 | 0 | 0 | 0 | 0 | 100 | 0 | 0 | 0 | 0 | 0 | 96.65 | 0 | 1.12 | 2.23 | 0 | 0 | 0 | 100 | 0 | 0 | 1.27 | 0 | 0 | 95.55 | 0 | 3.18 | 1.67 | 0 | 0 | 0 | 98.33 | 0 | 0 | 0 | 0 | 0 | 100 | 0 | 0.56 | 0 | 2.23 | 0 | 0 | 97.21 | 4.46 | 0 | 1.27 | 3.82 | 0 | 90.45 |
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