Table 4.

Aircraft sensors fault cases adopted in this paper.

Case	Sensor	Fault Type	Magnitude *
5	${\beta }_m$	extra noise	$5^{\circ }$∼${10}^{\circ }$
4	${\beta }_m$	drift	$\pm (5^{\circ }$∼${10}^{\circ })$
3	${\alpha }_m$	extra noise	$5^{\circ }$∼${10}^{\circ }$
2	${\alpha }_m$	drift	$\pm (5^{\circ }$∼${10}^{\circ })$
1	$V_m$	drift	$-(50\%$∼$100\%)$
0	clean measurement with noises and disturbances, no fault

* Noise standard deviation and drift values defined in this column.