A High-<italic>Q</italic> InP Resonant Angular Velocity Sensor for a Monolithically Integrated Optical Gyroscope

The design, fabrication, and optical characterization of the sensing element of a photonic InP-based gyroscope intended for applications in the field of aerospace and defense are reported in this paper. The sensing element is a spiral resonator coupled to a straight bus waveguide through a multimode...

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Main Authors: Caterina Ciminelli, Domenico DAgostino, Giuseppe Carnicella, Francesco DellOlio, Donato Conteduca, Huub P. M. M. Ambrosius, Meint K. Smit, Mario N. Armenise
Format: Article
Language:English
Published: IEEE 2016-01-01
Series:IEEE Photonics Journal
Subjects:
Online Access:https://ieeexplore.ieee.org/document/7352311/
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spelling doaj-1976380a7f7f43eca7ebd40f8974998f2021-03-29T17:29:34ZengIEEEIEEE Photonics Journal1943-06552016-01-018111910.1109/JPHOT.2015.25075497352311A High-<italic>Q</italic> InP Resonant Angular Velocity Sensor for a Monolithically Integrated Optical GyroscopeCaterina Ciminelli0Domenico DAgostino1Giuseppe Carnicella2Francesco DellOlio3Donato Conteduca4Huub P. M. M. Ambrosius5Meint K. Smit6Mario N. Armenise7Optoelectronics Laboratory, Department of Electrical and Information Engineering, Politecnico di Bari, Bari, ItalyInter-University Research School on Communication Technologies Basic Research and Applications (COBRA) Research Institute, Eindhoven University of Technology, Eindhoven, The NetherlandsOptoelectronics Laboratory, Department of Electrical and Information Engineering, Politecnico di Bari, Bari, ItalyOptoelectronics Laboratory, Department of Electrical and Information Engineering, Politecnico di Bari, Bari, ItalyOptoelectronics Laboratory, Department of Electrical and Information Engineering, Politecnico di Bari, Bari, ItalyInter-University Research School on Communication Technologies Basic Research and Applications (COBRA) Research Institute, Eindhoven University of Technology, Eindhoven, The NetherlandsInter-University Research School on Communication Technologies Basic Research and Applications (COBRA) Research Institute, Eindhoven University of Technology, Eindhoven, The NetherlandsOptoelectronics Laboratory, Department of Electrical and Information Engineering, Politecnico di Bari, Bari, ItalyThe design, fabrication, and optical characterization of the sensing element of a photonic InP-based gyroscope intended for applications in the field of aerospace and defense are reported in this paper. The sensing element is a spiral resonator coupled to a straight bus waveguide through a multimode interference coupler and exhibits a Q factor of approximately 600 000 with a footprint of approximately 10 mm <sup>2</sup>. The design of each component of the sensor is based on some well-established numerical methods such as the Finite Element Method, the beam propagation method, and the film mode matching method. The spiral cavity was designed using the standard transfer matrix method. The selected fabrication process, which is an enhanced version of the standard COBRA process, allows the monolithic integration of the sensing element with the other active components of the gyroscope, e.g., lasers, photodiodes, and modulators. Each component of the fabricated sensing element was optically characterized using an appropriate setup, which was also used for the optical characterization of the whole sensor. Based on the results of the characterization, the gyro performance was evaluated, and a way to improve both the resolution and the bias drift, i.e., down to 10&#x00B0;/h and 1&#x00B0;/h, respectively, was also clearly identified. The achieved results demonstrate, for the first time, the actual feasibility of a photonic gyro-on-chip through a well-established InP-based generic integration process.https://ieeexplore.ieee.org/document/7352311/Integrated opticsphotonic integrated circuitgeneric integration processoptical resonatorgyroscope
collection DOAJ
language English
format Article
sources DOAJ
author Caterina Ciminelli
Domenico DAgostino
Giuseppe Carnicella
Francesco DellOlio
Donato Conteduca
Huub P. M. M. Ambrosius
Meint K. Smit
Mario N. Armenise
spellingShingle Caterina Ciminelli
Domenico DAgostino
Giuseppe Carnicella
Francesco DellOlio
Donato Conteduca
Huub P. M. M. Ambrosius
Meint K. Smit
Mario N. Armenise
A High-<italic>Q</italic> InP Resonant Angular Velocity Sensor for a Monolithically Integrated Optical Gyroscope
IEEE Photonics Journal
Integrated optics
photonic integrated circuit
generic integration process
optical resonator
gyroscope
author_facet Caterina Ciminelli
Domenico DAgostino
Giuseppe Carnicella
Francesco DellOlio
Donato Conteduca
Huub P. M. M. Ambrosius
Meint K. Smit
Mario N. Armenise
author_sort Caterina Ciminelli
title A High-<italic>Q</italic> InP Resonant Angular Velocity Sensor for a Monolithically Integrated Optical Gyroscope
title_short A High-<italic>Q</italic> InP Resonant Angular Velocity Sensor for a Monolithically Integrated Optical Gyroscope
title_full A High-<italic>Q</italic> InP Resonant Angular Velocity Sensor for a Monolithically Integrated Optical Gyroscope
title_fullStr A High-<italic>Q</italic> InP Resonant Angular Velocity Sensor for a Monolithically Integrated Optical Gyroscope
title_full_unstemmed A High-<italic>Q</italic> InP Resonant Angular Velocity Sensor for a Monolithically Integrated Optical Gyroscope
title_sort high-<italic>q</italic> inp resonant angular velocity sensor for a monolithically integrated optical gyroscope
publisher IEEE
series IEEE Photonics Journal
issn 1943-0655
publishDate 2016-01-01
description The design, fabrication, and optical characterization of the sensing element of a photonic InP-based gyroscope intended for applications in the field of aerospace and defense are reported in this paper. The sensing element is a spiral resonator coupled to a straight bus waveguide through a multimode interference coupler and exhibits a Q factor of approximately 600 000 with a footprint of approximately 10 mm <sup>2</sup>. The design of each component of the sensor is based on some well-established numerical methods such as the Finite Element Method, the beam propagation method, and the film mode matching method. The spiral cavity was designed using the standard transfer matrix method. The selected fabrication process, which is an enhanced version of the standard COBRA process, allows the monolithic integration of the sensing element with the other active components of the gyroscope, e.g., lasers, photodiodes, and modulators. Each component of the fabricated sensing element was optically characterized using an appropriate setup, which was also used for the optical characterization of the whole sensor. Based on the results of the characterization, the gyro performance was evaluated, and a way to improve both the resolution and the bias drift, i.e., down to 10&#x00B0;/h and 1&#x00B0;/h, respectively, was also clearly identified. The achieved results demonstrate, for the first time, the actual feasibility of a photonic gyro-on-chip through a well-established InP-based generic integration process.
topic Integrated optics
photonic integrated circuit
generic integration process
optical resonator
gyroscope
url https://ieeexplore.ieee.org/document/7352311/
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