Abstract

In high-reliability applications, the health condition of the MEMS gyroscope needs to be known in real time to ensure that the system does not fail due to the wrong output signal. Because the MEMS gyroscope self-test based on the principle of electrostatic force cannot be performed during the working state. We propose that by monitoring the quadrature error signal of the MEMS gyroscope in real time, an online self-test of the MEMS gyroscope can be realized. The correlation between the gyroscope’s quadrature error amplitude signal and the gyroscope scale factor and bias was theoretically analyzed. Based on the sixteen-sided cobweb-like MEMS gyroscope, the real-time built-in self-test (BIST) method of the MEMS gyroscope based on the quadrature error signal was verified. By artificially setting the control signal of the gyroscope to zero, we imitated several scenarios where the gyroscope malfunctioned. Moreover, a mechanical impact table was used to impact the gyroscope. After a 6000 g shock, the gyroscope scale factor, bias, and quadrature error amplitude changed by −1.02%, −5.76%, and −3.74%, respectively, compared to before the impact. The gyroscope failed after a 10,000 g impact, and the quadrature error amplitude changed −99.82% compared to before the impact. The experimental results show that, when the amplitude of the quadrature error signal seriously deviates from the original value, it can be determined that the gyroscope output signal is invalid.

Highlights

  • In order to ensure the high reliability of MEMS gyroscope output data in highreliability applications, the researchers of MEMS gyroscopes improve the robustness of MEMS gyroscopes by enhancing the reliability design [1,2,3,4,5]

  • In order to ensure that the output of the MEMS gyroscope in high-reliability applications such as platform stability and inertial guidance is absolutely correct and reliable, we propose a simple way to achieve a real-time MEMS gyroscope self-test

  • By monitoring the change in the quadrature error amplitude in the working state, it can be inferred whether the gyroscope scale factor and bias have changed significantly, and it can be concluded whether the gyroscope output Coriolis signal is reliable

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Summary

Introduction

Publisher’s Note: MDPI stays neutral with regard to jurisdictional claims in published maps and institutional affiliations. In order to ensure the high reliability of MEMS gyroscope output data in highreliability applications, the researchers of MEMS gyroscopes improve the robustness of MEMS gyroscopes by enhancing the reliability design [1,2,3,4,5] They use fault detection methods to check the gyroscope’s state when the gyroscope is powered on or during its work [6,7,8,9]. In order to ensure that the output of the MEMS gyroscope in high-reliability applications such as platform stability and inertial guidance is absolutely correct and reliable, we propose a simple way to achieve a real-time MEMS gyroscope self-test. The sixth and seventh sections detail the MEMS gyroscope online BIST experiment and conclusion, respectively

The Quadrature Error Signal of the Gyroscope
The BIST Based on Quadrature Error
MEMS Gyroscope Design and Fabrication
The fabrication process flow of the a 6-inch wafer with 100 μm thick
Design
BIST Simulation of the MEMS Gyroscope
Gyroscope
The BIST Experiment
The Electric Malfunction Imitated Test
The Mechanical Shock Test
Discussion
Patents
Full Text
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