DFBW

By taking a verifying aircraft which is equipped with longitudinal DFBW as an example, this paper studied of influences to landing flying qualities for probable controlling mistake and pilot model parameters variations in the man-aircraft closed-loop system.

本文以装备纵向数字电传操纵系统（DFBW）的某验证机为实例，分析研究了该人-机闭环系统中驾驶员模型参数变化和可能出现的操纵差错对纵向着陆品质的影响。

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He problem of how to depress the limit cycle oscillation of flight control system must be solved in the design of DFBW system.

抑制飞控系统极限环振荡是设计数字电传系统时需要解决的重要问题。

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These conclusion are beneficial to new aircraft development and the pilots who are going to fly the aircraft equipped with DFBW.

这些结论对新机研制和即将驾驶装备DFBW飞机的驾驶员是十分有益的。

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A method of restrain self-sustaining oscillation in longitudinal DFBW of an aircraft

某飞机纵向DFBW自持振荡的抑制措施

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Longitudinal DFBW control law design for a certain act demonstration aircraft

某ACT验证机纵向DFBW控制律设计

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The control characteristics of longitudinal DFBW aircraft during landing process

纵向DFBW飞机着陆过程中的操纵特点

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