{"title":"空间应用的高精度光子晶体光纤陀螺仪","authors":"Xiaobin Xu, Ningfang Song, Zhihao Zhang, Wei Cai, Fuyu Gao","doi":"10.1364/ACPC.2017.SU1A.3","DOIUrl":null,"url":null,"abstract":"A low-loss (∼1.7dB/km) PM-PCF has been designed and fabricated, based on which a PCFOG having a bias stability of ∼0.002°/h is developed. The PCFOG has a flight test in \"Tianzhou-1\" Cargo Spaceship.","PeriodicalId":285199,"journal":{"name":"2017 Asia Communications and Photonics Conference (ACP)","volume":"92 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2017-11-10","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"7","resultStr":"{\"title\":\"High Precision Photonic Crystal Fiber Optic Gyroscope for Space Application\",\"authors\":\"Xiaobin Xu, Ningfang Song, Zhihao Zhang, Wei Cai, Fuyu Gao\",\"doi\":\"10.1364/ACPC.2017.SU1A.3\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"A low-loss (∼1.7dB/km) PM-PCF has been designed and fabricated, based on which a PCFOG having a bias stability of ∼0.002°/h is developed. The PCFOG has a flight test in \\\"Tianzhou-1\\\" Cargo Spaceship.\",\"PeriodicalId\":285199,\"journal\":{\"name\":\"2017 Asia Communications and Photonics Conference (ACP)\",\"volume\":\"92 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2017-11-10\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"7\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2017 Asia Communications and Photonics Conference (ACP)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1364/ACPC.2017.SU1A.3\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2017 Asia Communications and Photonics Conference (ACP)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1364/ACPC.2017.SU1A.3","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
High Precision Photonic Crystal Fiber Optic Gyroscope for Space Application
A low-loss (∼1.7dB/km) PM-PCF has been designed and fabricated, based on which a PCFOG having a bias stability of ∼0.002°/h is developed. The PCFOG has a flight test in "Tianzhou-1" Cargo Spaceship.
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