gust alleviation control

基本解释

The wing has a two-spar structure and an active control surface for gust response alleviation.
該機翼具有雙梁式結搆和一個用於陣風響應減緩的主動控制麪。
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It shows that the designed control law is effective for flutter suppression and gust alleviation.
風洞實騐結果表明：設計控制律具有抑制顫振和減緩陣風響應的雙重功能。
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.
用該方法對某主動控制飛機的垂直平移模態（直接力控制）進行了解耦設計，竝將其應用於飛機的陣風減緩。