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民用飞机偏航控制系统设计策略
引用本文:伊鹤鹤,王培文.民用飞机偏航控制系统设计策略[J].飞机设计,2021,41(6):24-28.
作者姓名:伊鹤鹤  王培文
作者单位:(西飞民用飞机有限责任公司,陕西西安710089)
摘    要:偏航控制系统是保证飞机安全飞行的关键系统,方向舵是偏航控制主要操纵面.针对方向舵主-主-主余度配置,设计其权限管理和故障重构策略;针对偏航阻尼功能闭环控制方式的特点,设计其指令表决及弹性模态之间的不良耦合规避策略;实现一种高安全性和高可靠性的偏航控制系统.

关 键 词:偏航控制  权限管理  故障重构  指令表决  弹性模态
收稿时间:2020/10/4 0:00:00
修稿时间:2021/9/19 0:00:00

Control Strategy Yaw Control System for Civil Aircraft
YI Hehe,WANG Peiwen.Control Strategy Yaw Control System for Civil Aircraft[J].Aircraft Design,2021,41(6):24-28.
Authors:YI Hehe  WANG Peiwen
Institution:(XAC Commercial Aircraft Co.,Ltd.,Xi''an 710089,China)
Abstract:The yaw control system is the critical system to ensure the safe flight of aircraft, and therudder is the main surface of the yaw control. Aiming at the rudder surface active-active-active configuration , its authority management and fault re-configuration strategy were designed. In terms of thecharacteristics of the closed-loop control mode of the yaw damper function, its commanding votinglogic and evasion strategy of the elastic mode were designed and a high safety and high reliability ofthe yaw control system.
Keywords:yaw control  authority management  fault re-configuration  command voting  elasticmode
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