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基于上抛式四脉冲方案的原子干涉陀螺设计与实现

The design and implementation of an atom interference gyroscope based on four-pulse atomic-fountain scheme

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【作者】 牛克骁; 王宇晨; 刘元正; 岳亚洲; 鲍淑宁; 吴彬;

【Author】 NIU Kexiao;WANG Yuchen;LIU Yuanzheng;YUE Yazhou;BAO Shuning;WU Bin;Flight Automatic Control Research Institute;Aviation Key Laboratory of Science and Technology on Quantum Sensing and Positioning Navigation Timing;Zhejiang University of Technology;

【机构】 西安飞行自动控制研究所; 量子传感与定位导航授时技术航空科技重点实验室; 浙江工业大学;

【摘要】 原子干涉陀螺仪是目前已知的理论精度最高的陀螺仪,近年来国内外各研究机构提出了多种不同的系统架构和实现方案。设计并实现了一种基于上抛式四脉冲方案的原子干涉陀螺仪,其在同等体积下能够实现更高的角速度测量精度。分析了其基本原理,设计了高精度角速度测量实验流程,通过改变拉曼激光频率差操控原子干涉路径正向和反向交替运行,进一步提升系统性能。最后对系统静态性能进行分析,得到其零偏稳定性为0.029(°)/h(1σ,100 s@室温),角度随机游走为2.06×10-6 rad/s/Hz1/2,零偏不稳定性为1.65×10-8 rad/s。

【Abstract】 Atom interferometry gyroscopes(AIG) currently represent the highest theoretically achievable precision in gyroscopic technology. In recent years, various system architectures and implementation schemes have been proposed by domestic and international research institutions. An four-pulse atomic fountain type based atom interferometry gyroscope has been designed and implemented, demonstrating superior angular velocity measurement accuracy under identical volumetric constraints. The fundamental principles are analyzed, and a high-precision angular velocity measurement experimental process is designed. System performance is further improved by alternating the Raman laser frequency difference to manipulate the atomic interference paths between forward and reverse operational modes. Finally, the static performance analysis demonstrates a bias stability of 0.029(°)/h(1σ, 100 s @room temperature), with an angular random walk of 2.06×10-6 rad/s/Hz1/2 and bias instability reaching 1.66×10-8 rad/s.

【基金】 国家自然科学基金(U2341246)
  • 【文献出处】 中国惯性技术学报 ,Journal of Chinese Inertial Technology , 编辑部邮箱 ,2025年12期
  • 【分类号】TH824.3
  • 【下载频次】28
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