Navigation grade mems imu for a satellite

34Citations
Citations of this article
24Readers
Mendeley users who have this article in their library.

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.

Cite

CITATION STYLE

APA

Zhao, W., Cheng, Y., Zhao, S., Hu, X., Rong, Y., Duan, J., & Chen, J. (2021). Navigation grade mems imu for a satellite. Micromachines, 12(2), 1–12. https://doi.org/10.3390/mi12020151

Register to see more suggestions

Mendeley helps you to discover research relevant for your work.

Already have an account?

Save time finding and organizing research with Mendeley

Sign up for free