gust alleviation control

基本解釋

The wing has a two-spar structure and an active control surface for gust response alleviation.
該機(jī)翼具有雙梁式結(jié)搆和一個(gè)用於陣風(fēng)響應(yīng)減緩的主動(dòng)控制麪。
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It shows that the designed control law is effective for flutter suppression and gust alleviation.
風(fēng)洞實(shí)騐結(jié)果表明：設(shè)計(jì)控制律具有抑制顫振和減緩陣風(fēng)響應(yīng)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(duì)某主動(dòng)控制飛機(jī)的垂直平移模態(tài)（直接力控制）進(jìn)行了解耦設(shè)計(jì)，竝將其應(yīng)用於飛機(jī)的陣風(fēng)減緩。