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冗余配置捷联惯性导航系统可靠性分析 被引量:5

Reliability Analysis for a Redundant Strapdown Inertial Navigation System
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摘要 采用容错技术提高导航系统的可靠性是现代导航技术主要发展方向之一,采用冗余敏感器配置的捷联惯导系统具有成本低、重量轻和可靠性高等优点。利用马尔可夫模型对四余度双轴冗余惯性敏感器配置的导航组件的可靠性进行建模,对敏感器质量、故障检测和故障隔离的误差(包括误警率、漏检率和故障隔离率等)、系统任务时间和系统其它部件的故障概率等因素对导航系统可靠性的影响进行了分析和比较。 Fault diagnosis has become an issue of primary importance in modern navigation.The redundant strapdoun inertial navigation system has many merit points, such as cheap,light and reliable. In the reliability analyzing, Markov process theory can by applied to describe the original working condition of the system. In the paper, the effects of different system parameters on the reliability of a redundant strapdown system were assessed
出处 《航天控制》 CSCD 北大核心 1999年第3期71-77,共7页 Aerospace Control
基金 "九五"国防预研基金
关键词 惯性导航系统 可靠性分析 冗余技术 捷联式 Inertial guidance system Reliability analysis Redundancy technique
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参考文献2

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同被引文献31

  • 1钱华明.冗余技术在惯性组合导航系统中的应用研究[J].中国惯性技术学报,1999,7(1):11-14. 被引量:2
  • 2王珍熙.捷联式惯性导航系统惯性元件的设置与可靠性[J].中国惯性技术学报,1996,4(1):63-67. 被引量:6
  • 3郭秀中.惯导系统陀螺仪理论[M].北京:国防工业出版社,1996..
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  • 6陈哲.捷联惯导原理[M].北京:宇航出版社,1986..
  • 7WANG W. A joint spare part and maintenance inspection optimization model using the delay-time concept [ J 1. Reli- ability Engineering and System Safety, 2011,96 ( 11 ) : 1535-1541.
  • 8WANG W. An inspection model based on a three-stage failure process [ J ]. Reliability Engineering and System Safety, 2011,96 ( 7 ) : 838 -848.
  • 9SHARAREH T, DRAGAN B. Optimum inspection interval for a system under periodic and opportunistic inspections [ J]. IIE Transactions,2012,44( 11 ) :932-948.
  • 10YUAN W ZH, XU G Q. Optimal repair policy for a system with two unit deteriorating standby system [ C ]. Control Conference ( CCC), Yantai, China,2011 : 1871-1876.

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