考虑结冰对临界迎角、升阻特性等的影响，通过建立非线性动力学仿真模型和特殊情况下驾驶员操纵副翼偏转模型，实现了机翼结冰后的人-机系统动态仿真。
In order to quantitatively analyze the flight risk for wing icing, the probability assessment was proposed in which the simulation data of the pilot-aircraft-environment system was utilized.
考虑结冰对临界迎角、升阻特性等的影响，通过建立非线性动力学仿真模型和特殊情况下驾驶员操纵副翼偏转模型，实现了机翼结冰后的人-机系统动态仿真。
In order to quantitatively analyze the flight risk for wing icing, the probability assessment was proposed in which the simulation data of the pilot-aircraft-environment system was utilized.
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