{"title":"CubeSat兼容光纤陀螺仪","authors":"Hung-Pin Chung, Sheng-Han Chang, Ching-Lu Hsieh, Sung-Lin Yang, Yen-Hung Chen","doi":"10.1109/OECC48412.2020.9273677","DOIUrl":null,"url":null,"abstract":"We report the design, construction, and test of a compact fiber-optic gyroscope (FOG) for cost-effective low-earth-orbit CubeSat applications. This medium-grade FOG is developed by the integration of a miniaturized (16-mm long) multifunction integrated optic circuit and a streamlined feedback electric-optical control logic module. The whole structure layout of the FOG has been carefully designed and optimized to effectively reduce the weight of the unit in a 1U (10x10x10 cm3) space.","PeriodicalId":433309,"journal":{"name":"2020 Opto-Electronics and Communications Conference (OECC)","volume":"7 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2020-10-04","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"CubeSat compatible Fiber-Optic Gyroscope\",\"authors\":\"Hung-Pin Chung, Sheng-Han Chang, Ching-Lu Hsieh, Sung-Lin Yang, Yen-Hung Chen\",\"doi\":\"10.1109/OECC48412.2020.9273677\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"We report the design, construction, and test of a compact fiber-optic gyroscope (FOG) for cost-effective low-earth-orbit CubeSat applications. This medium-grade FOG is developed by the integration of a miniaturized (16-mm long) multifunction integrated optic circuit and a streamlined feedback electric-optical control logic module. The whole structure layout of the FOG has been carefully designed and optimized to effectively reduce the weight of the unit in a 1U (10x10x10 cm3) space.\",\"PeriodicalId\":433309,\"journal\":{\"name\":\"2020 Opto-Electronics and Communications Conference (OECC)\",\"volume\":\"7 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2020-10-04\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2020 Opto-Electronics and Communications Conference (OECC)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/OECC48412.2020.9273677\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2020 Opto-Electronics and Communications Conference (OECC)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/OECC48412.2020.9273677","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
We report the design, construction, and test of a compact fiber-optic gyroscope (FOG) for cost-effective low-earth-orbit CubeSat applications. This medium-grade FOG is developed by the integration of a miniaturized (16-mm long) multifunction integrated optic circuit and a streamlined feedback electric-optical control logic module. The whole structure layout of the FOG has been carefully designed and optimized to effectively reduce the weight of the unit in a 1U (10x10x10 cm3) space.
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