电磁环境下飞行控制系统传感器的故障容忍度

17th DASC. AIAA/IEEE/SAE. Digital Avionics Systems Conference. Proceedings (Cat. No.98CH36267) Pub Date : 1998-10-31 DOI:10.1109/DASC.1998.741551

J. Suh, B. Chang, A. Lau

{"title":"电磁环境下飞行控制系统传感器的故障容忍度","authors":"J. Suh, B. Chang, A. Lau","doi":"10.1109/DASC.1998.741551","DOIUrl":null,"url":null,"abstract":"High Intensity Radiated Field (HIRE) conditions may cause sensor and/or controller failure in flight control system. In this paper, a flight dynamics imitation scheme is proposed to establish the failure tolerance of sensors in Electro-Magnetic Environment (EME).","PeriodicalId":335827,"journal":{"name":"17th DASC. AIAA/IEEE/SAE. Digital Avionics Systems Conference. Proceedings (Cat. No.98CH36267)","volume":"41 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"1998-10-31","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Failure tolerance of sensors in flight control systems in electromagnetic environment\",\"authors\":\"J. Suh, B. Chang, A. Lau\",\"doi\":\"10.1109/DASC.1998.741551\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"High Intensity Radiated Field (HIRE) conditions may cause sensor and/or controller failure in flight control system. In this paper, a flight dynamics imitation scheme is proposed to establish the failure tolerance of sensors in Electro-Magnetic Environment (EME).\",\"PeriodicalId\":335827,\"journal\":{\"name\":\"17th DASC. AIAA/IEEE/SAE. Digital Avionics Systems Conference. Proceedings (Cat. No.98CH36267)\",\"volume\":\"41 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"1998-10-31\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"17th DASC. AIAA/IEEE/SAE. Digital Avionics Systems Conference. Proceedings (Cat. No.98CH36267)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/DASC.1998.741551\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"17th DASC. AIAA/IEEE/SAE. Digital Avionics Systems Conference. Proceedings (Cat. No.98CH36267)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/DASC.1998.741551","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}

引用次数: 0

摘要

在飞行控制系统中，高强度辐射场(HIRE)条件可能导致传感器和/或控制器失效。为了建立电磁环境下传感器的容错能力，提出了一种飞行动力学仿真方案。

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

Failure tolerance of sensors in flight control systems in electromagnetic environment

High Intensity Radiated Field (HIRE) conditions may cause sensor and/or controller failure in flight control system. In this paper, a flight dynamics imitation scheme is proposed to establish the failure tolerance of sensors in Electro-Magnetic Environment (EME).

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

17th DASC. AIAA/IEEE/SAE. Digital Avionics Systems Conference. Proceedings (Cat. No.98CH36267)

自引率

0.00%

发文量