飞机导航与着陆无线电电子系统诊断准确性的估计方法

2018 IEEE 5th International Conference on Methods and Systems of Navigation and Motion Control (MSNMC) Pub Date : 2018-10-01 DOI:10.1109/MSNMC.2018.8576269

I. Machalin, I. Terentyeva, A. Taranenko, Ye. I. Gabrousenko

{"title":"飞机导航与着陆无线电电子系统诊断准确性的估计方法","authors":"I. Machalin, I. Terentyeva, A. Taranenko, Ye. I. Gabrousenko","doi":"10.1109/MSNMC.2018.8576269","DOIUrl":null,"url":null,"abstract":"The method for estimation of veracity of the diagnostics of an aircraft landing and navigation radio-electronic system dismantled units is given in this article. It considers the stimulating signals source instability and the object of diagnosis reliability. Settlement formulas are offered for an assessment of the veracity indicators. These formulas take into account specifics of the aircraft landing and navigation system diagnosis device.","PeriodicalId":404334,"journal":{"name":"2018 IEEE 5th International Conference on Methods and Systems of Navigation and Motion Control (MSNMC)","volume":"79 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2018-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"2","resultStr":"{\"title\":\"Method for Estimation the Veracity of Diagnosis of the Aircraft Navigation and Landing Radio-Electronic Systems\",\"authors\":\"I. Machalin, I. Terentyeva, A. Taranenko, Ye. I. Gabrousenko\",\"doi\":\"10.1109/MSNMC.2018.8576269\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"The method for estimation of veracity of the diagnostics of an aircraft landing and navigation radio-electronic system dismantled units is given in this article. It considers the stimulating signals source instability and the object of diagnosis reliability. Settlement formulas are offered for an assessment of the veracity indicators. These formulas take into account specifics of the aircraft landing and navigation system diagnosis device.\",\"PeriodicalId\":404334,\"journal\":{\"name\":\"2018 IEEE 5th International Conference on Methods and Systems of Navigation and Motion Control (MSNMC)\",\"volume\":\"79 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2018-10-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"2\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2018 IEEE 5th International Conference on Methods and Systems of Navigation and Motion Control (MSNMC)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/MSNMC.2018.8576269\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2018 IEEE 5th International Conference on Methods and Systems of Navigation and Motion Control (MSNMC)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/MSNMC.2018.8576269","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}

引用次数: 2

摘要

本文给出了飞机着舰导航无线电电子系统拆装单元诊断准确性的估计方法。它考虑了激励信号源的不稳定性和诊断对象的可靠性。给出了沉降公式，用于评价准确性指标。这些公式考虑了飞机着陆和导航系统诊断装置的具体情况。

本文章由计算机程序翻译，如有差异，请以英文原文为准。

查看原文本刊更多论文

Method for Estimation the Veracity of Diagnosis of the Aircraft Navigation and Landing Radio-Electronic Systems

The method for estimation of veracity of the diagnostics of an aircraft landing and navigation radio-electronic system dismantled units is given in this article. It considers the stimulating signals source instability and the object of diagnosis reliability. Settlement formulas are offered for an assessment of the veracity indicators. These formulas take into account specifics of the aircraft landing and navigation system diagnosis device.

求助全文

通过发布文献求助，成功后即可免费获取论文全文。去求助

来源期刊

2018 IEEE 5th International Conference on Methods and Systems of Navigation and Motion Control (MSNMC)

自引率

0.00%

发文量