{"title":"Design and implementation of calibration circuit for crystal oscillator","authors":"Qiu Fang, Shanzhu Xiao, Huan-zhang Lu, Yabei Wu","doi":"10.1109/ICAM.2016.7813576","DOIUrl":null,"url":null,"abstract":"High performance crystal oscillator is usually used as the clock source of system timer in a miniaturization space aircraft, however, it cannot overcome the effect of long-term aging on accuracy. Thus, this paper presents a simple, light and efficient circuit to calibrate the difference between the actual output frequency and the nominal frequency of a crystal oscillator periodically in real time. The experiments show that the proposed design reduces the timing deviation from more than 1614ms to less than 1ms in 5 hours. The timing error is less than the required error index, which gives strong support to the working timer of a space aircraft.","PeriodicalId":179100,"journal":{"name":"2016 International Conference on Integrated Circuits and Microsystems (ICICM)","volume":"73 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2016-11-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"1","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"2016 International Conference on Integrated Circuits and Microsystems (ICICM)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/ICAM.2016.7813576","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 1
Abstract
High performance crystal oscillator is usually used as the clock source of system timer in a miniaturization space aircraft, however, it cannot overcome the effect of long-term aging on accuracy. Thus, this paper presents a simple, light and efficient circuit to calibrate the difference between the actual output frequency and the nominal frequency of a crystal oscillator periodically in real time. The experiments show that the proposed design reduces the timing deviation from more than 1614ms to less than 1ms in 5 hours. The timing error is less than the required error index, which gives strong support to the working timer of a space aircraft.