Wing/horizontal tail ice shape regulation and control optimization method, system, equipment and medium

The invention discloses a wing/horizontal tail ice shape regulation and control optimization method, system and device and a medium. The method comprises the steps that S1, pneumatic data of a wing/horizontal tail under different regulation and control ice shapes are obtained; s2, calculating and quantifying a dynamic safety boundary according to the pneumatic data to obtain dynamic safety boundary quantitative indexes under different regulation and control ice shapes; and S3, selecting the maximum value in the dynamic safety boundary quantitative indexes to arrange an anti-icing/de-icing device. Technical support can be provided for optimizing arrangement of the wing/horizontal tail ice preventing and removing device, and then flight safety is improved. 本发明公开了一种机翼/平尾冰形调控优化方法、系统、设备及介质，S1，获取机翼/平尾不同调控冰形下的气动数据；S2，根据气动数据计算并量化动力学安全边界，得到不同调控冰形下的动力学安全边界量化指标；S3，选择动力学安全边界量化指标中的最大值来布置防/除冰装置。能够为优化机翼/平尾防除冰装置布置提供技术支撑，进而提升飞行安全。