Research Article
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 |
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