In this paper a longitudinal robust automatic landing control law was designed by QFT approach combine with thrust controls.
采用QFT理论设计了某型飞机的纵向着陆控制律，并应用了推力综合控制稳定飞机下滑时的速度。
In this paper a longitudinal robust automatic landing control law was designed by QFT approach combine with thrust controls.
采用QFT理论设计了某型飞机的纵向着陆控制律，并应用了推力综合控制稳定飞机下滑时的速度。
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