Encountering a verticalgust environment the plane will get unexpectful longitudinal load.
飞机受到垂直阵风的影响会产生不希望的法向过载。
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 gust alleviation.
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 optimization requires the minimization of the vertical overload at the pilot′s seat, the attitude variation and the control energy consumption under the gust disturbance.