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

Table 8

NLGA Monte Carlo analysis with 𝑝=10 and 𝑟_fa%.

Faulty sensor	𝑟mf	𝑟td	𝑟ti, 𝜏md	𝜏mi, 𝛿𝑒
0.003	0.004	0.996	30	𝛿𝑎 s
0.002	0.002	0.998	15	𝛿𝑟 s
0.001	0.001	0.999	23	𝛿th s
0.004	0.003	0.997	32	𝜈=5 s