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作 者:FANG JianCheng QIN Jie WAN ShuangAi CHEN Yao LI RuJie
机构地区:[1]Science and Technology on Inertial Laboratory,Beihang University
出 处:《Chinese Science Bulletin》2013年第13期1512-1515,共4页
基 金:supported by the National Natural Science Foundation of China (60825305, 61121003);the National Basic Research Program of China (2009CB724002);the Defense Industrial Technology Development Program of China (B2120110002)
摘 要:Atomic spin gyroscope (ASG) based on comagnetometer is a high sensitive and compact gyroscope for future inertial navigation applications. The start-up time was several hours of the demonstrated ASGs based on 3He-K or21 Ne-Rb-K comagnetometer, and only a few inertial navigation applications allow such a long time for preparation. We report the demonstration of an ASG based on 129Xe-Cs comagnetometer, which decreases the start-up time to 10 minutes and decreases the operation temperature by 40% as well. By operating this ASG in spin exchange relaxation free regime, a sensitivity of 7×10 -5 °/(s Hz1/2) was achieved.Atomic spin gyroscope (ASG) based on comagnetometer is a high sensitive and compact gyroscope for future inertial navigation applications. The start-up time was several hours of the demonstrated ASGs based on 3He-K or 21Ne-Rb-K comagnetometer, and only a few inertial navigation applications allow such a long time for preparation. We report the demonstration of an ASG based on 129Xe-Cs comagnetometer, which decreases the start-up time to 10 minutes and decreases the operation temperature by 40% as well. By operating this ASG in spin exchange relaxation free regime, a sensitivity of 7x10-5 (s Hz1/2) was achieved.
关 键 词:自旋交换 陀螺仪 原子 CS 高灵敏度 惯性导航 启动时间 应用程序
分 类 号:TN966[电子电信—信号与信息处理]
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