This paper presents an approach to possibility of directforcecontrol on the joined wing configuration.
对连接翼气动布局实现直接力控制的可能性进行了初步的探索。
2
The disadvantages of normal aircraft in flight path control can be overcome by using directforcecontrol, and some new motion modes can be realized.
采用直接力控制可弥补常规飞机在轨迹操纵方面的不足， 并产生某些新的运动模式。
3
The disadvantages of normal aircraft to realize flight path control can be overcome by using directforcecontrol, and some new motion modes can be created.