Robust Data-Driven Fault Detection: An Application to Aircraft Air Data Sensors

Table 1

Different aircraft and flight conditions adopted in this paper.

Aircraft	General configuration	Weight	Span	Data source	Flight condition
	Large cargo airplane, quadruple piston engines, high wing	41.0 t	38.0 m	Simulation	(i) Low altitude, LTO, manual
	Large passenger aircraft, quadruple turbo engines, low wing	174 t	59.6 m	Simulation	(i) High altitude, cruise, AP; (ii) Low altitude, free flight, manual
	Large passenger aircraft, double turbo engines, low wing	44.6 t	35.8 m	Real flight	(i) Low altitude, LTO, manual
	General aviation, double piston engines, high wing	3.12 t	19.8 m	Simulation	(i) High altitude, cruise, AP
	Fighter aircraft, double turbo engines, delta wing	10.5 t	11.4 m	Real flight	(i) Medium altitude, manual flight