摘要
针对电传飞行控制系统法向加速度传感器故障监控方法进行研究,通过模型监控的方法对法向加速度传感器进行故障诊断与隔离,从而提高电传飞行控制系统的可靠性。
In this paper, the fault monitoring method for normal acceleration sensors of fly-by-wire flight control system is researched. To improve reliability of FBW flight control system, the monitoring model method is used for fault diagnosis and isolation of normal acceleration sensors.
出处
《教练机》
2014年第1期62-64,共3页
Trainer
关键词
模型监控
电传飞行控制系统
法向加速度传感器
可靠性
model monitoring
fly-by-wire flight control system
normal acceleration sensors
reliability