Research Article

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

Table 7

PM Monte Carlo analysis with 𝑝 = 1 0 and 𝑟 f a %.

Faulty sensor 𝑟 m f 𝑟 t d 𝑟 t i , 𝜏 m d 𝜏 m i , 𝛿 𝑒

0 . 0 0 2 0 . 0 0 3 0 . 9 9 7 2 7 𝛿 𝑎  s
0 . 0 0 1 0 . 0 0 1 0 . 9 9 9 1 8 𝛿 𝑟  s
0 . 0 0 2 0 . 0 0 3 0 . 9 9 7 2 5 𝛿 t h  s
0 . 0 0 3 0 . 0 0 2 0 . 9 9 8 3 5 𝜈 = 1 2  s