On Flight Risk Quantitative Evaluation under Icing Conditions

Table 1

Data goodness of fit for simulation of pilot model and real pilot.

Extreme parameters	Correlation coefficient	K-S	P value	R-square
Extreme minimum airspeed	0.9607	0.0850	0.4486	0.9230
Extreme roll angle	0.9797	0.0450	0.9855	0.9599
Extreme AOA	0.9667	0.1050	0.2078	0.9346