Abstract

This paper presents microfabrication process-driven design of a multi-degree of freedom (multi-DoF) non-resonant electrostatic microelectromechanical systems (MEMS) gyroscope by considering the design constraints of commercially available low-cost and widely-used silicon-on-insulator multi-user MEMS processes (SOIMUMPs), with silicon as a structural material. The proposed design consists of a 3-DoF drive mode oscillator with the concept of addition of a collider mass which transmits energy from the drive mass to the passive sense mass. In the sense direction, 2-DoF sense mode oscillator is used to achieve dynamically-amplified displacement in the sense mass. A detailed analytical model for the dynamic response of MEMS gyroscope is presented and performance characteristics are validated through finite element method (FEM)-based simulations. The effect of operating air pressure and temperature variations on the air damping and resulting dynamic response is analyzed. The thermal stability of the design and corresponding effect on the mechanical and capacitive sensitivity, for an operating temperature range of −40 °C to 100 °C, is presented. The results showed that the proposed design is thermally stable, robust to environmental variations, and process tolerances with a wide operational bandwidth and high sensitivity. Moreover, a system-level model of the proposed gyroscope and its integration with the sensor electronics is presented to estimate the voltage sensitivity under the constraints of the readout electronic circuit.

Highlights

  • The gyroscopes detect rotation of an object and are an integral part of Inertial Measurement Units (IMUs) which enable the development of self-contained and high precision Inertial Navigation Systems (INSs)

  • We present the design of a multi-DoF non-resonant electrostatic microelectromechanical systems (MEMS) gyroscope with 3-DoF drive and 2-DoF sense mode oscillators to achieve both wide operational bandwidth and high mechanical sensitivity

  • We have presented a design of a 3-DoF drive mode and 2-DoF sense mode vibratory MEMS gyroscope considering the design rules of commercially available multi-user foundry process SOIMUMPs

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Summary

Introduction

The gyroscopes detect rotation of an object and are an integral part of Inertial Measurement Units (IMUs) which enable the development of self-contained and high precision Inertial Navigation Systems (INSs). The main drawback of this two-mass system-based approach is that the operational bandwidth and mechanical gain of the MEMS gyroscope can only be increased by optimizing the mass and resonant frequency ratio of masses that are coupled together To overcome this issue, a modified vibration absorber design concept has been proposed in [16] with the addition of a grounded mechanical spring that is attached to the absorber mass. The sensitivity values vary in units owing to the fact that in the literature either mechanical, capacitive or voltage sensitivity values are reported for a respective MEMS gyroscope design Most of these designs utilize a multi-DoF design concept in either the drive or sense mode, but not in both

Microfabrication Process
Analytical Modeling of the Multi-DoF MEMS Gyroscope
Air Damping Analysis
Pull-in Voltage AnMaolydseisShape
Effect of Operating Temperature and Pressure Variations on MEMS Gyroscope
Thermal Stability Analysis of MEMS Gyroscope
Analysis of Fabrication Process Tolerances on Frequency Response
Mechanical Sensitivity Analysis
Findings
Discussion
Conclusions
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