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

Table 3

PM FDI technique: minimal ramp faults with 𝑐_𝑖(𝑡).

𝛿𝑒	Variable	Fault size	Delay time
Elevator	0.11^∘/s	26	𝛿𝑎 s
Aileron	0.50^∘/s	11	𝛿𝑟 s
Rudder	0.49^∘/s	12	𝛿th s
Throttle aperture %	0.13^∘/s	19	𝐾𝛿th=1 s