Constructing and characterizing a novel MEMS-based Tuning Fork Gyroscope using PolyMUMPs

Selvakumar, V. S.; Sujatha, L.; Balasubramanian, Vishal

doi:10.1007/s00542-020-05129-5

Cited by 3 publications

(2 citation statements)

References 17 publications

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“…The structure can be actuated by electrostatic, piezoelectric, or magnetic forces, and the angular rate is detected by capacitive, piezoelectric, or piezoresistive methods [1][2][3]. To actuate and sense, electrostatic and capacitive methods have been used as they are widely used due to their simplicity, low power usage, and easy integration with MEMS structures.…”

Section: Mems Gyroscope's Working Principle and Structural Designmentioning

confidence: 99%

“…Microelectromechanical system (MEMS) gyroscopes are inertial sensors used for measuring the angular velocity of an object by using the Coriolis effect. In the past two decades, resonant MEMS gyroscopes have attracted significant attention from both academia and industry because of their advantages of compact size, high sensitivity, low power usage, low fabrication cost, and bulk production [1][2][3][4]. At the start of the 21st century, research on MEMS gyroscopes began to advance, paving the way for practical design implementations [4].…”

Section: Introductionmentioning

confidence: 99%

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Design and analysis of mode-matched decoupled mass MEMS gyroscope with improved thermal stability

Bashir,

Bazaz,

Saleem

et al. 2024

Meas. Sci. Technol.

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This paper presents an efﬁcient design approach for microelectromechanical systems (MEMS) gyroscope considering the design constraint of MEMSCAP's Silicon-on-Insulator Multi-User MEMS Processes (SOIMUMPs). A design for a decoupled mass MEMS resonant gyroscope with tuning electrodes is presented to minimize cross-axis coupling and optimize the gyroscope's performance. The device features a size of 1.8 ×2.772 mm^2. A decoupled mass MEMS gyroscope has been designed using a novel mechanical beam configuration that optimizes the structural design to reduce unwanted interactions between drive and sense axes motions. Mode order has been achieved by obtaining the first two modes as drive and sense modes at 9946.3 Hz and 10202.7 Hz, respectively. Parallel plate electrostatic tuning electrodes have been added to adjust and match the drive and sense modes at the resonant frequencies of 9946 Hz. This mode matching is crucial for optimizing gyroscope performance, accuracy, and sensitivity. The effects of temperature variation on the performance of the designed decoupled mass MEMS gyroscope have been investigated, particularly in terms of its mode-matched operation achieved using tuning electrodes. Finite Element Method (FEM) simulations were conducted, demonstrating that thermal stability was achieved, and mode-matched operation was maintained within the temperature range of -40 ºC to 80 ºC. The gyroscope exhibits enhanced performance compared to existing MEMS gyroscopes under mode-matched conditions, featuring a lower temperature coefficient of frequency (TCF) at 0.0415 Hz/ºC in the drive mode and 0.0165 Hz/ºC in the sense mode. FEM analysis for the fabrication process tolerances has been done, where MEMS gyroscope’s resonant frequencies, output capacitance, output displacement, and sense mode quality factor have shown negligible changes to fabrication process tolerances. Transient analysis was conducted using CoventorWare MEMS+ 3D schematic, which was integrated with MATLAB Simulink to measure the MEMS gyroscope’s output response, which corresponded with the varying input angular velocity signal.

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Section: Mems Gyroscope's Working Principle and Structural Designmentioning

confidence: 99%