Some progress is being made with MEMS Inertial Measurement Units (IMUs) for spacecraft use:
Navigation Grade MEMS IMU for A Satellite
Wanliang Zhao, Yuxiang Cheng, Sihan Zhao, Xiaomao Hu, Yijie Rong, Jie Duan and Jiawei Chen
Micromachines 2021, 12, 151.
https://doi.org/10.3390/mi12020151 Published: 4 February 2021
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 °/√h. It is the highest precision MEMS IMU for commercial aerospace use ever publicly reported in the world to date.
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The Lobster-Eye X-ray Satellite employed a MEMS IMU and a navigation grade fiber optic gyroscope (FOG) unit weighing 430 g. The in-orbit data of the MEMS unit transmitted from the satellite and the FOG unit almost completely overlap each other, as displayed in Figure 10, which means that the output and control effect of the MEMS IMU is similar to that of the FOG unit on the same satellite. Meanwhile, the weight and volume of the MEMS unit are only about 1/2 of the FOG unit.