Design and Analysis of Robust Fault Diagnosis Schemes for a Simulated Aircraft Model

Table 9

NN Monte Carlo analysis with 𝑟_fa.

Faulty sensor	𝑟mf	𝑟td	𝑟ti, 𝜏md	𝜏mi, 𝛿𝑒
0.004	0.005	0.995	33	𝛿𝑎 s
0.003	0.003	0.997	23	𝛿𝑟 s
0.004	0.004	0.996	29	𝛿th s
0.005	0.003	0.997	38	𝜈=9 s