Literature DB >> 33557116

Navigation Grade MEMS IMU for A Satellite.

Wanliang Zhao1, Yuxiang Cheng1, Sihan Zhao1, Xiaomao Hu1, Yijie Rong1, Jie Duan1, Jiawei Chen1.   

Abstract

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 °/h1/2. It is the highest precision MEMS IMU for commercial aerospace use ever publicly reported in the world to date.

Entities:  

Keywords:  IMU; MEMS gyroscopes; commercial aerospace; navigation grade; satellite

Year:  2021        PMID: 33557116     DOI: 10.3390/mi12020151

Source DB:  PubMed          Journal:  Micromachines (Basel)        ISSN: 2072-666X            Impact factor:   2.891


  2 in total

Review 1.  MEMS Inertial Sensor Calibration Technology: Current Status and Future Trends.

Authors:  Xu Ru; Nian Gu; Hang Shang; Heng Zhang
Journal:  Micromachines (Basel)       Date:  2022-05-31       Impact factor: 3.523

2.  Online Compensation of Phase Delay Error Based on P-F Characteristic for MEMS Vibratory Gyroscopes.

Authors:  Xuewen Liu; Zhengcheng Qin; Hongsheng Li
Journal:  Micromachines (Basel)       Date:  2022-04-19       Impact factor: 3.523

  2 in total

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