direct lift control

基本解釋

This paper presents an approach to the direct lift control characteristics on the joined wing configuration.
本文對(duì)聯(lián)接翼氣動(dòng)布局的直接升力控制特性進(jìn)行了初步的探索。
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)，并將其應(yīng)用于飛機(jī)的陣風(fēng)減緩。
According to the characters of Dynamic Inversion method in making multivariable control system decoupling, we design a set of control law for every direct lift control mode.
本文針對(duì)動(dòng)態(tài)逆控制方法的不足之處提出了相應(yīng)的改善措施，并取得了較為理想的效果。