The basic modes of directliftcontrol are analyzed in this paper.
本文对联接翼气动布局的直接升力控制特性进行了初步的探索。
2
As a numerical example, we used our method to design the vertical transition mode(directliftcontrol) 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
According to the characters of Dynamic Inversion method in making multivariable control system decoupling, we design a set of control law for every directliftcontrol mode.