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

Table 1

Nomenclature.

𝛼	Angle of attack
𝛽	Angle of sideslip
𝑝𝜔	Roll rate
𝑞𝜔	Pitch rate
𝑟𝜔	Yaw rate
𝜙	Bank angle
𝜃	Elevation angle
𝜓	Heading angle
𝑛𝑒	Engine shaft angular rate
[^𝐼𝑥0−𝐼𝑥𝑧0𝐼𝑦^0−𝐼𝑥𝑧0𝐼𝑧]	Inertia moment matrix
𝑉	True airspeed (TAS)
𝛿𝑒	Elevator deflection angle
𝛿𝑎	Aileron deflection angle
𝛿𝑟	rudder deflection angle
𝛿th	Throttle aperture percentage
𝐻	Altitude
𝛾	Flight path angle
𝑚	Airplane mass
𝜔𝑢, 𝜔𝑣, 𝜔𝑤	Wind gust components