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arXiv 2008.05602physics.ins-detastro-ph.IMphysics.optics
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用于精密惯性传感的单元件双干涉仪

Single-element dual-interferometer for precision inertial sensing

Yichao Yang, Kohei Yamamoto, Victor Huarcaya, Christoph Vorndamme, Daniel Penkert, Germán Fernández Barranco, Thomas S Schwarze, Juan Jose Esteban Delgado, Mori… 展开作者

Yichao Yang, Kohei Yamamoto, Victor Huarcaya, Christoph Vorndamme, Daniel Penkert, Germán Fernández Barranco, Thomas S Schwarze, Juan Jose Esteban Delgado, Moritz Mehmet, Jianjun Jia, Gerhard Heinzel, Miguel Dovale Álvarez

AI总结:

本文提出自参考单元件双干涉仪(SEDI)惯性传感器,通过深度频率调制干涉测量在单个光学元件中集成两个干涉仪,实现紧凑封装下的亚皮米级高精度惯性传感,适用于天基无拖曳控制和地基惯性隔离系统。

摘要:

以高精度和大动态范围在多个自由度上跟踪运动质量是许多当前和未来引力物理实验的核心方面。激光干涉仪已被确立为此类测量方案的优选工具之一。使用正弦相位调制零差干涉法可以大幅降低光学装置结构的复杂性,而结构复杂性是多通道干涉测量的一个关键限制。通过将装置结构的复杂性转移到信号处理阶段,这些方法使设备能够达到传统技术无法实现的尺寸和重量。在本文中,我们提出了一种基于深度频率调制干涉测量的新型传感器拓扑设计:自参考单元件双干涉仪(SEDI)惯性传感器,它通过在一个光学元件中容纳两个干涉仪,将简化又向前推进了一步。结合计算机模型和分析方法,我们表明,在几立方英寸的封装内,对于10 mHz以上的频率,具有亚皮米精度的惯性传感器用我们的方法似乎是可行的。此外,我们表明,通过组合两个此类设备,有可能在低至2 mHz的频率下达到亚皮米精度。结合所具备的紧凑性,这使得SEDI传感器成为一种有前景的方法,可用于高精度惯性传感应用,既适用于采用无拖曳控制的下一代天基引力任务,也适用于采用光学读出的惯性隔离系统的地基实验。

英文摘要:

Tracking moving masses in several degrees of freedom with high precision and large dynamic range is a central aspect in many current and future gravitational physics experiments. Laser interferometers have been established as one of the tools of choice for such measurement schemes. Using sinusoidal phase modulation homodyne interferometry allows a drastic reduction of the complexity of the optical setup, a key limitation of multi-channel interferometry. By shifting the complexity of the setup to the signal processing stage, these methods enable devices with a size and weight not feasible using conventional techniques. In this paper we present the design of a novel sensor topology based on deep frequency modulation interferometry: the self-referenced single-element dual-interferometer (SEDI) inertial sensor, which takes simplification one step further by accommodating two interferometers in one optic. Using a combination of computer models and analytical methods we show that an inertial sensor with sub-picometer precision for frequencies above 10 mHz, in a package of a few cubic inches, seems feasible with our approach. Moreover we show that by combining two of these devices it is possible to reach sub-picometer precision down to 2 mHz. In combination with the given compactness, this makes the SEDI sensor a promising approach for applications in high precision inertial sensing for both next-generation space-based gravity missions employing drag-free control, and ground-based experiments employing inertial isolation systems with optical readout.

机构、总结、中文摘要均由AI分析而来,可能存在错误,请以论文正文为准。

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