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Navigation Grade MEMS IMU for A Satellite

This paper presents a navigation grade micro-electromechanical system (MEMS) inertial measurement unit (IMU) that was successfully applied for the first time in the Lobster-Eye X-ray Satellite in July 2020. A six-axis MEMS gyroscope redundant configuration is adopted in the unit to improve the perfo...

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Detalles Bibliográficos
Autores principales: Zhao, Wanliang, Cheng, Yuxiang, Zhao, Sihan, Hu, Xiaomao, Rong, Yijie, Duan, Jie, Chen, Jiawei
Formato: Online Artículo Texto
Lenguaje:English
Publicado: MDPI 2021
Materias:
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC7913845/
https://www.ncbi.nlm.nih.gov/pubmed/33557116
http://dx.doi.org/10.3390/mi12020151
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author Zhao, Wanliang
Cheng, Yuxiang
Zhao, Sihan
Hu, Xiaomao
Rong, Yijie
Duan, Jie
Chen, Jiawei
author_facet Zhao, Wanliang
Cheng, Yuxiang
Zhao, Sihan
Hu, Xiaomao
Rong, Yijie
Duan, Jie
Chen, Jiawei
author_sort Zhao, Wanliang
collection PubMed
description This paper presents a navigation grade micro-electromechanical system (MEMS) inertial measurement unit (IMU) that was successfully applied for the first time in the Lobster-Eye X-ray Satellite in July 2020. A six-axis MEMS gyroscope redundant configuration is adopted in the unit to improve the performance through mutual calibration of a set of two-axis gyroscopes in the same direction. In the paper, a satisfactory precision of the gyroscope is achieved by customized and self-calibration gyroscopes whose parameters are adjusted at the expense of bandwidth and dynamics. According to the in-orbit measured data, the MEMS IMU provides an outstanding precision of better than 0.02 °/h (1σ) with excellent bias instability of 0.006 °/h and angle random walk (ARW) of around 0.003 °/h(1/2). It is the highest precision MEMS IMU for commercial aerospace use ever publicly reported in the world to date.
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spelling pubmed-79138452021-02-28 Navigation Grade MEMS IMU for A Satellite Zhao, Wanliang Cheng, Yuxiang Zhao, Sihan Hu, Xiaomao Rong, Yijie Duan, Jie Chen, Jiawei Micromachines (Basel) Article This paper presents a navigation grade micro-electromechanical system (MEMS) inertial measurement unit (IMU) that was successfully applied for the first time in the Lobster-Eye X-ray Satellite in July 2020. A six-axis MEMS gyroscope redundant configuration is adopted in the unit to improve the performance through mutual calibration of a set of two-axis gyroscopes in the same direction. In the paper, a satisfactory precision of the gyroscope is achieved by customized and self-calibration gyroscopes whose parameters are adjusted at the expense of bandwidth and dynamics. According to the in-orbit measured data, the MEMS IMU provides an outstanding precision of better than 0.02 °/h (1σ) with excellent bias instability of 0.006 °/h and angle random walk (ARW) of around 0.003 °/h(1/2). It is the highest precision MEMS IMU for commercial aerospace use ever publicly reported in the world to date. MDPI 2021-02-04 /pmc/articles/PMC7913845/ /pubmed/33557116 http://dx.doi.org/10.3390/mi12020151 Text en © 2021 by the authors. Licensee MDPI, Basel, Switzerland. This article is an open access article distributed under the terms and conditions of the Creative Commons Attribution (CC BY) license (http://creativecommons.org/licenses/by/4.0/).
spellingShingle Article
Zhao, Wanliang
Cheng, Yuxiang
Zhao, Sihan
Hu, Xiaomao
Rong, Yijie
Duan, Jie
Chen, Jiawei
Navigation Grade MEMS IMU for A Satellite
title Navigation Grade MEMS IMU for A Satellite
title_full Navigation Grade MEMS IMU for A Satellite
title_fullStr Navigation Grade MEMS IMU for A Satellite
title_full_unstemmed Navigation Grade MEMS IMU for A Satellite
title_short Navigation Grade MEMS IMU for A Satellite
title_sort navigation grade mems imu for a satellite
topic Article
url https://www.ncbi.nlm.nih.gov/pmc/articles/PMC7913845/
https://www.ncbi.nlm.nih.gov/pubmed/33557116
http://dx.doi.org/10.3390/mi12020151
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