降低InP混合光学陀螺仪后向散射噪声的实验对策

F. Dell’Olio, F. Indiveri, F. Innone, C. Ciminelli, M. Armenise
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引用次数: 3

摘要

目前可用的中高性能角速度传感器的小型化对航空航天和国防工业至关重要。为了应对这一技术挑战,我们正在研究一种基于InP光子集成电路技术的新型陀螺仪,称为片上陀螺仪(GoC)。我们提到的传感器包括一个Q大于一百万的无源环形谐振器和几个光学/光电元件,它们都是单片集成在单个InP芯片上的。本文介绍了GoC论证的最新进展。特别讨论了读出电路的结构和对后向散射噪声的抑制措施。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Experimental countermeasures to reduce the backscattering noise in an InP hybrid optical gyroscope
Miniaturization of the currently available medium- and high-performance angular velocity sensors is crucial for aerospace and defense industry. To face this technological challenge, we are investigating a new gyro, called gyroscope-on-chip (GoC), based on the InP photonic integrated circuits technology. The sensor we refer includes a passive ring resonator with a Q greater than one million and several optical/optoelectronic components all monolithically integrated on a single InP chip. Recent progress on the demonstration of the GoC is reported in this paper. In particular, the configuration of the readout circuit and the countermeasures against the backscattering noise are discussed.
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