This article are of reference value to extend gustalleviation technique to engineering application.
本文的工作对工程实际中采用阵风减缓技术具有参考价值。
2
As a numerical example, we used our method to design the vertical transition mode(direct lift control) of a certain active-control aircraft for gustalleviation.
用该方法对某主动控制飞机的垂直平移模态(直接力控制)进行了解耦设计,并将其应用于飞机的阵风减缓。
3
The wing has a two-spar structure and an active control surface for gust response alleviation.