{"title":"自修复飞行控制系统可靠性评估覆盖模型","authors":"Tijian Chen","doi":"10.1109/AEROCS.1993.720970","DOIUrl":null,"url":null,"abstract":"This paper reports a coverage model for assessing the overall reliability of self-repairing flight control systems where the performance of an FDIA (Failure Detection, Isolation and Accommodation) logic is involved. Provided that each of the N parallel redundant components is of the same exponential failure probability and non-repairable on-line, it has been proved that the resulting failure process can be described by a homogeneous Markov chain model if the failure can be identified perfectly by the FDIA scheme used, otherwise the process is non-homogeneous. Furthermore, for either homogeneous or non-homogeneous case approximation of computing the failure transition probability and the corresponding error have been derived.","PeriodicalId":170527,"journal":{"name":"Proceedings. The First IEEE Regional Conference on Aerospace Control Systems,","volume":"PP 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"1993-05-25","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Coverage Modelling for Reliability Assessment Self-Repairing Flight Control Systems\",\"authors\":\"Tijian Chen\",\"doi\":\"10.1109/AEROCS.1993.720970\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"This paper reports a coverage model for assessing the overall reliability of self-repairing flight control systems where the performance of an FDIA (Failure Detection, Isolation and Accommodation) logic is involved. Provided that each of the N parallel redundant components is of the same exponential failure probability and non-repairable on-line, it has been proved that the resulting failure process can be described by a homogeneous Markov chain model if the failure can be identified perfectly by the FDIA scheme used, otherwise the process is non-homogeneous. Furthermore, for either homogeneous or non-homogeneous case approximation of computing the failure transition probability and the corresponding error have been derived.\",\"PeriodicalId\":170527,\"journal\":{\"name\":\"Proceedings. The First IEEE Regional Conference on Aerospace Control Systems,\",\"volume\":\"PP 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"1993-05-25\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Proceedings. The First IEEE Regional Conference on Aerospace Control Systems,\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/AEROCS.1993.720970\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Proceedings. The First IEEE Regional Conference on Aerospace Control Systems,","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/AEROCS.1993.720970","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Coverage Modelling for Reliability Assessment Self-Repairing Flight Control Systems
This paper reports a coverage model for assessing the overall reliability of self-repairing flight control systems where the performance of an FDIA (Failure Detection, Isolation and Accommodation) logic is involved. Provided that each of the N parallel redundant components is of the same exponential failure probability and non-repairable on-line, it has been proved that the resulting failure process can be described by a homogeneous Markov chain model if the failure can be identified perfectly by the FDIA scheme used, otherwise the process is non-homogeneous. Furthermore, for either homogeneous or non-homogeneous case approximation of computing the failure transition probability and the corresponding error have been derived.