{"title":"提高航天器热控系统地面试验参数估计可靠性的方法","authors":"V. Belova","doi":"10.17238/ISSN2409-0239.2015.4.74","DOIUrl":null,"url":null,"abstract":". The paper considers the automated technique for modeling and calculation of reliability (probability of failure-free operation ) system for thermal control system of transport cargo ship “Progress”. The technique is based on the logical-probabilistic methodology flowcharts reliability, fault tree and Markov modeling implemented in specialized programs Windchill Quality Solutions software version 10.2 (previously , Relex).","PeriodicalId":436954,"journal":{"name":"Rocket-Space Device Engineering and Information Systems","volume":"51 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2015-12-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"1","resultStr":"{\"title\":\"Methodology for Improving the Reliability of Parameters Estimates of Spacecraft Thermal Control System during Ground Tests\",\"authors\":\"V. Belova\",\"doi\":\"10.17238/ISSN2409-0239.2015.4.74\",\"DOIUrl\":null,\"url\":null,\"abstract\":\". The paper considers the automated technique for modeling and calculation of reliability (probability of failure-free operation ) system for thermal control system of transport cargo ship “Progress”. The technique is based on the logical-probabilistic methodology flowcharts reliability, fault tree and Markov modeling implemented in specialized programs Windchill Quality Solutions software version 10.2 (previously , Relex).\",\"PeriodicalId\":436954,\"journal\":{\"name\":\"Rocket-Space Device Engineering and Information Systems\",\"volume\":\"51 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2015-12-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"1\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Rocket-Space Device Engineering and Information Systems\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.17238/ISSN2409-0239.2015.4.74\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Rocket-Space Device Engineering and Information Systems","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.17238/ISSN2409-0239.2015.4.74","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Methodology for Improving the Reliability of Parameters Estimates of Spacecraft Thermal Control System during Ground Tests
. The paper considers the automated technique for modeling and calculation of reliability (probability of failure-free operation ) system for thermal control system of transport cargo ship “Progress”. The technique is based on the logical-probabilistic methodology flowcharts reliability, fault tree and Markov modeling implemented in specialized programs Windchill Quality Solutions software version 10.2 (previously , Relex).
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