期刊文献+

冗余捷联惯组故障重构策略研究 被引量:6

Research on Reconfiguration Strategy and Structure for Redundant IMU
原文传递
导出
摘要 针对因漏警率和参数不确定性所引起的多传感器融合精度损失进行数学建模并开展研究。首先对高低精度两传感器融合模型给出分析,进而对三正交一斜置配置给出斜表是否参与融合的精度影响分析。分析表明在考虑漏警率等因素的前提下,所有惯性表均参与估计有精度损失风险。基于所构建的模型给出冗余捷联惯组的重构策略,在策略的指导下提出双三正交架构,并与正十二面体配置进行对比。对比结果表明双三正交在无故障和一度故障下性能和正十二面体配置相当,考虑不确定性,双三正交架构有一定优势。 The accuracy of multi-sensor fusion considering with fail alarm and uncertainty is analyzed. Firstly, the fusion of two sensors with different precision are investigated. Then, the impact is analyzed whether the fusion includes skew axe for the configuration of three orthogonal axes and one skew axe. It is shown that the presence of fail alarm and the fusion accuracy would not improve but get worse, including all sensors' uncertainty. A more appropriate reconfiguration strategy based on the built model is presented. A structure of dual triads is proposed under the guidance of strategy and compared with the configuration of dodecahedron. It is proved that the optimal performance of two structures is almost equal in the absence of failure and one sensor failure. A structure of dual triads has its advantages considering uncertainty and computation complexity.
作者 周维正 赵赛君 李学锋 Zhou Weizheng;Zhao Saijun;Li Xuefeng(Beijing Aerospace Automatic Control Institute,Beijing 100854,China;Beijing Institute of Radio Measurement,Beijing 100854,China)
出处 《战术导弹技术》 北大核心 2018年第5期68-72,共5页 Tactical Missile Technology
关键词 捷联惯组 重构策略 冗余容错 双三正交架构 strapdown IMU reconfiguration strategy redundancy fault-tolerant structure of dualtriads
  • 相关文献

参考文献3

二级参考文献16

  • 1Kevin C,Daly,F( )ai and James V,Harrison.Generalized likelihood test for FDI in redundant sensor configurations[J].Guidance and Control,1978,2(1):9-17
  • 2Biao Huang.Detection of abrupt change of total least squares models and application in fault detection[J].IEEE Transactions on Control Systems Technology,2001,9(2):357-367
  • 3Duk-Sun Shim,Cheol-Kwan Yang.Geometric FDI based on SVD for redundant inertial sensor systems[J].2004 5th Asian Control Conference,2004,6:1094-1100
  • 4D.M.哈兰;R.D.罗伦茨;阎列;邓宁丰;舒承东.航天系统故障与对策[M]北京:宇航出版社,2007.
  • 5Daly K C,Gai E and Harrison J V Generalized likelihood test for FDI in rendundant sensor configurations[J].Journal of Guidance and Control,1979,2(2):9-17.
  • 6Hirokimi S.Study on strapdown inertial navigation redundant sensor system[J].NALTR-660.1981—03.
  • 7Harrison J V,Gai E G.Evaluating sensor orientantions for navigation performance and failureDetection[J].IEEE Transaction on Aerospace and Electronic System,1977,AES_13(6):631-643.
  • 8Yuksel Y. Design and analysis of inertial navigation systems with skew redundant inertial sensors[D].Canada:University of Calgary,2011.
  • 9颜东,张洪钺.均值检验方法及其在冗余惯性导航系统中的应用[J].航空学报,1997,18(4):417-422. 被引量:5
  • 10李伶.双捷联冗余控制系统中的加速度计及陀螺仪判别方法研究[J].航天控制,1998,16(2):2-9. 被引量:7

共引文献27

同被引文献44

引证文献6

二级引证文献14

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部