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

Table 5

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

𝛿𝑒	Variable	Fault size	Delay time
Elevator	0.21^∘/s	11	𝛿𝑎 s
Aileron	0.45^∘/s	12	𝛿𝑟 s
Rudder	0.32^∘/s	10	𝛿th s
Throttle aperture %	0.15^∘/s	15	4 s