On Flight Risk Quantitative Evaluation under Icing Conditions

Table 5

Fitting test of extreme roll angle.

Model	K-S		A-D		χ2
EV	0.1590	0.0001	10.3930	0	15.1128
GEV	0.0295	0.9931	0.1976	0.9911	0.0921
Long	0.0345	0.9650	0.2201	0.9839	0.0876
Weibull	0.0876	0.0876	3.0570	0.0256	1.4002
Exp	0.3942	<0.0001	43.5374	<0.0001	17.6790
Norm	0.0788	0.1583	2.8350	0.0333	1.2308