{"title":"定制航天器电力系统兼容性的电磁干扰规范","authors":"Richard W. Boettcher, Alan K. Johnson","doi":"10.1109/ISEMC.1979.7568850","DOIUrl":null,"url":null,"abstract":"An analysis procedure is described for use in determining the steady-state EMC margin in a spacecraft primary power distribution system. The analysis begins with estimates of broadband and narrowband emissions from each equipment unit. These are combined at the power source impedance to produce a bus ripple voltage spectrum which is then compared to the equipment susceptibility specification. Thus, the three variables of emission, susceptibility and source impedance are related in such a manner that specification tailoring can be performed and design tradeoffs can be evaluated.","PeriodicalId":283257,"journal":{"name":"1979 IEEE International Symposium on Electromagnetic Compatibility","volume":"12 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"1979-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Tailoring EMI Specifications for Spacecraft Electrical Power System Compatibility\",\"authors\":\"Richard W. Boettcher, Alan K. Johnson\",\"doi\":\"10.1109/ISEMC.1979.7568850\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"An analysis procedure is described for use in determining the steady-state EMC margin in a spacecraft primary power distribution system. The analysis begins with estimates of broadband and narrowband emissions from each equipment unit. These are combined at the power source impedance to produce a bus ripple voltage spectrum which is then compared to the equipment susceptibility specification. Thus, the three variables of emission, susceptibility and source impedance are related in such a manner that specification tailoring can be performed and design tradeoffs can be evaluated.\",\"PeriodicalId\":283257,\"journal\":{\"name\":\"1979 IEEE International Symposium on Electromagnetic Compatibility\",\"volume\":\"12 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"1979-10-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"1979 IEEE International Symposium on Electromagnetic Compatibility\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/ISEMC.1979.7568850\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"1979 IEEE International Symposium on Electromagnetic Compatibility","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/ISEMC.1979.7568850","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Tailoring EMI Specifications for Spacecraft Electrical Power System Compatibility
An analysis procedure is described for use in determining the steady-state EMC margin in a spacecraft primary power distribution system. The analysis begins with estimates of broadband and narrowband emissions from each equipment unit. These are combined at the power source impedance to produce a bus ripple voltage spectrum which is then compared to the equipment susceptibility specification. Thus, the three variables of emission, susceptibility and source impedance are related in such a manner that specification tailoring can be performed and design tradeoffs can be evaluated.
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