{"title":"基于锂离子电池和COTS集成电路的先进微卫星集成电池模块","authors":"C. Del Vecchio Blanco, M. D'Errico","doi":"10.1109/AERO.2004.1368074","DOIUrl":null,"url":null,"abstract":"A six Li-ion cell string is used as the core of a modular battery for a total 100 Wh@C/2 capacity and a Wh efficiency of about 90%. Integrated charge/discharge prototype electronics is based on COTS components which allows us to obtain an efficiency greater than 90% and negligible mass and volume. Electronics can be managed by an integrated microcontroller which can by reprogrammed by the on-board computer. Battery management is foreseen at three levels: local battery module, power conditioning unit and on-board computer.","PeriodicalId":208052,"journal":{"name":"2004 IEEE Aerospace Conference Proceedings (IEEE Cat. No.04TH8720)","volume":"19 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2004-03-13","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"2","resultStr":"{\"title\":\"Integrated battery module based on Li-ion cells and COTS ICs for advanced microsatellites\",\"authors\":\"C. Del Vecchio Blanco, M. D'Errico\",\"doi\":\"10.1109/AERO.2004.1368074\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"A six Li-ion cell string is used as the core of a modular battery for a total 100 Wh@C/2 capacity and a Wh efficiency of about 90%. Integrated charge/discharge prototype electronics is based on COTS components which allows us to obtain an efficiency greater than 90% and negligible mass and volume. Electronics can be managed by an integrated microcontroller which can by reprogrammed by the on-board computer. Battery management is foreseen at three levels: local battery module, power conditioning unit and on-board computer.\",\"PeriodicalId\":208052,\"journal\":{\"name\":\"2004 IEEE Aerospace Conference Proceedings (IEEE Cat. No.04TH8720)\",\"volume\":\"19 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2004-03-13\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"2\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2004 IEEE Aerospace Conference Proceedings (IEEE Cat. No.04TH8720)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/AERO.2004.1368074\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2004 IEEE Aerospace Conference Proceedings (IEEE Cat. No.04TH8720)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/AERO.2004.1368074","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Integrated battery module based on Li-ion cells and COTS ICs for advanced microsatellites
A six Li-ion cell string is used as the core of a modular battery for a total 100 Wh@C/2 capacity and a Wh efficiency of about 90%. Integrated charge/discharge prototype electronics is based on COTS components which allows us to obtain an efficiency greater than 90% and negligible mass and volume. Electronics can be managed by an integrated microcontroller which can by reprogrammed by the on-board computer. Battery management is foreseen at three levels: local battery module, power conditioning unit and on-board computer.
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