{"title":"用于下一代航天器动力系统的无set、全数字负载点调节器","authors":"Nijad Anabtawi, Rabih Chamoun","doi":"10.1109/AERO.2016.7500865","DOIUrl":null,"url":null,"abstract":"This paper presents a digitally controlled point-of-load regulator for next-generation power systems. It is intended for spacecraft with limited energy harvesting capability and on board battery storage such as micro- and nano-satellites as well as multi-tier power distribution networks of conventional satellite and spacecraft subsystems. The novel control loop was designed to minimize radiation induced single-event effects (SEE) and resulting transients. The design was implemented in 14nm bulk complimentary metal-oxide semiconductor (CMOS) process and validated with post layout simulations. It attains a peak efficiency of 95% at heavy load conditions and 79% at light loads with a maximum voltage ripple of 25mV at light loads. The most susceptible elements of the proposed regulator have a relatively high energy threshold (~ 15pJ corresponding to 40 MeV.cm2/mg) indicating a small probability of occurrence in harsh environments and no catastrophic failure.","PeriodicalId":150162,"journal":{"name":"2016 IEEE Aerospace Conference","volume":"33 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2016-03-05","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"1","resultStr":"{\"title\":\"An SET-free, fully-digital point-of-load regulator for next-generation spacecraft power systems\",\"authors\":\"Nijad Anabtawi, Rabih Chamoun\",\"doi\":\"10.1109/AERO.2016.7500865\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"This paper presents a digitally controlled point-of-load regulator for next-generation power systems. It is intended for spacecraft with limited energy harvesting capability and on board battery storage such as micro- and nano-satellites as well as multi-tier power distribution networks of conventional satellite and spacecraft subsystems. The novel control loop was designed to minimize radiation induced single-event effects (SEE) and resulting transients. The design was implemented in 14nm bulk complimentary metal-oxide semiconductor (CMOS) process and validated with post layout simulations. It attains a peak efficiency of 95% at heavy load conditions and 79% at light loads with a maximum voltage ripple of 25mV at light loads. The most susceptible elements of the proposed regulator have a relatively high energy threshold (~ 15pJ corresponding to 40 MeV.cm2/mg) indicating a small probability of occurrence in harsh environments and no catastrophic failure.\",\"PeriodicalId\":150162,\"journal\":{\"name\":\"2016 IEEE Aerospace Conference\",\"volume\":\"33 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2016-03-05\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"1\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2016 IEEE Aerospace Conference\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/AERO.2016.7500865\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2016 IEEE Aerospace Conference","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/AERO.2016.7500865","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
An SET-free, fully-digital point-of-load regulator for next-generation spacecraft power systems
This paper presents a digitally controlled point-of-load regulator for next-generation power systems. It is intended for spacecraft with limited energy harvesting capability and on board battery storage such as micro- and nano-satellites as well as multi-tier power distribution networks of conventional satellite and spacecraft subsystems. The novel control loop was designed to minimize radiation induced single-event effects (SEE) and resulting transients. The design was implemented in 14nm bulk complimentary metal-oxide semiconductor (CMOS) process and validated with post layout simulations. It attains a peak efficiency of 95% at heavy load conditions and 79% at light loads with a maximum voltage ripple of 25mV at light loads. The most susceptible elements of the proposed regulator have a relatively high energy threshold (~ 15pJ corresponding to 40 MeV.cm2/mg) indicating a small probability of occurrence in harsh environments and no catastrophic failure.