Reducing the Sensitivity of Fabrication Error in the MEMS Butterfly Gyroscope by Adopting an Improved Vibration Beam
Author:
Affiliation:
1. College of Intelligence Science and Technology, National University of Defense Technology, Changsha, China
Funder
National Key Research and Development Program of China
Publisher
Institute of Electrical and Electronics Engineers (IEEE)
Subject
Electrical and Electronic Engineering,Instrumentation
Link
http://xplorestaging.ieee.org/ielx7/7361/10068826/10040619.pdf?arnumber=10040619
Reference21 articles.
1. 0.00016 deg/√hr Angle Random Walk (ARW) and 0.0014 deg/hr Bias Instability (BI) from a 5.2M-Q and 1-cm Precision Shell Integrating (PSI) Gyroscope
2. Overview and analysis of MEMS Coriolis vibratory ring gyroscope
3. Ultrafast laser in fabrication of micro hemispherical resonators with quality factor over millions
4. Effect of Electrode Design on Frequency Tuning in Shell Resonators
5. A quadrature compensation method to improve the performance of the butterfly vibratory gyroscope
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1. Monolithic Integrated Interface ASIC With Quadrature Error Correction for MEMS Dual-Mass Vibration Gyroscope;IEEE Sensors Journal;2024-06-01
2. Design of an interface circuit system for mode-separation MEMS digital gyroscope;Modern Physics Letters B;2023-12-12
3. Adaptive Fuzzy Modal Matching of Capacitive Micromachined Gyro Electrostatic Controlling;Sensors;2023-08-25
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