首页 | 本学科首页   官方微博 | 高级检索  
     

飞行传感器的故障检测与识别
引用本文:张洪钺. 飞行传感器的故障检测与识别[J]. 航空学报, 1991, 12(10): 494-502
作者姓名:张洪钺
作者单位:北京航空航天大学
摘    要: 飞行传感器是飞行控制和导航系统中的薄弱环节,它们的故障率一般是比较高的。为了提高系统的可靠性,对传感器的故障应能实时地检测和识别,并重构传感器所测量的信号(修正)。为此,在系统中常采用传感器的硬件余度和解析余度。本文介绍了飞行传感器硬件余度和解析余度的原理以及几种实用的余度方案,对解析余度中的统计决策原理和故障检测的鲁棒性问题也作了简单介绍。

关 键 词:故障检测和识别  解析余度  系统可残性  

FAILURE DETECTION AND IDENTIFICATION FOR AIRCRAFT SENSORS
Beijing University of Aeronautics and Astronautics Zhang Hongyue. FAILURE DETECTION AND IDENTIFICATION FOR AIRCRAFT SENSORS[J]. Acta Aeronautica et Astronautica Sinica, 1991, 12(10): 494-502
Authors:Beijing University of Aeronautics and Astronautics Zhang Hongyue
Affiliation:Beijing University of Aeronautics and Astronautics Zhang Hongyue
Abstract:Aircraft sensors are less reliable components in flight control and navigation systems, In order to improve the system reliability, it is desired to detect and identify the faulty sensor and reconstruct the signal measured by the sensor in real time. Hardware and analytieal redundancy are adopted for this purpose. In this paper, a comprehensive survey is given to the analytical redundancy technology. Numerous schemes of analytical redundancy for aircraft sensors are introduced. The principle of statistical decision making for analytical redundancy and the robustness of failure detection and identification algorithms are discussed briefly.
Keywords:Failure detection and identification   analytical redundancy   System reli- ability
本文献已被 CNKI 等数据库收录!
点击此处可从《航空学报》浏览原始摘要信息
点击此处可从《航空学报》下载全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号