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

Table 10

UIKF Monte Carlo analysis with 𝑟_fa.

Faulty sensor	𝑟mf	𝑟td	𝑟ti, 𝜏md	𝜏mi, 𝛿𝑒
0.003	0.004	0.996	26	𝛿𝑎 s
0.002	0.002	0.998	17	𝛿𝑟 s
0.001	0.002	0.998	26	𝛿th s
0.004	0.003	0.997	37	0.6 s