Advanced Multiobjective Structure Optimization and Excitation Method of Metal Resonant Gyro

The metal resonant gyro is characterized by small size, low cost, and strong overload resistance, and shows broad application prospects in the field of inertial navigation. Currently, structural optimization methods of resonators are based on single-objective parameter optimization and fail to consider the comprehensive impact of multiple structural parameters on overall performance indices. In this paper, a metal resonator with a tooth structure is designed based on thin shell theory and the energy loss principle. Using a finite element simulation method combined with multivariate linear regression equations, the linear influence of each structural parameter on overall performance is investigated. A multi-objective optimization model using three key indices as objective functions is constructed and optimized with the NSGA-II algorithm, providing a set of optimization parameters for subsequent research. It establishes equivalent mathematical models for different forms of electrostatic forces and verify their validity using finite element simulations. Finally, the resonator’s response under different excitation forms is experimentally validated. Results show that the resonator exhibits optimal resonance under single-octave sinusoidal excitation: the four-wave belly oscillation pattern remains intact in driving mode with no frequency crosstalk. The resonant amplitude limit is 0.34 nm, significantly greater than under other excitation forms. The proposed method achieves comprehensive performance optimization of the metal resonator and provides a theoretical basis for selecting excitation forms in resonant gyros.

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Publication Details

Journal
IEEE Transactions on Instrumentation and Measurement
Published
2025-01-01
DOI
https://doi.org/10.1109/tim.2025.3557121
Citations
1
Primary Topic
Inertial Sensor and Navigation
Type
article
Field-Weighted Citation Impact
4.99

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article

Advanced Multiobjective Structure Optimization and Excitation Method of Metal Resonant Gyro

Zhong Su, Taochen Gu, Xuesi Yang, Lianxi Zheng et al.
1 citations
IEEE Transactions on Instrumentation and Measurement
Inertial Sensor and Navigation
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article

Advanced Multiobjective Structure Optimization and Excitation Method of Metal Resonant Gyro

Zhong Su, Taochen Gu, Xuesi Yang, Lianxi Zheng, Zhenyu Zhao, Ning Liu, Wensong Wang
article en
1 citations

Abstract

The metal resonant gyro is characterized by small size, low cost, and strong overload resistance, and shows broad application prospects in the field of inertial navigation. Currently, structural optimization methods of resonators are based on single-objective parameter optimization and fail to consider the comprehensive impact of multiple structural parameters on overall performance indices. In this paper, a metal resonator with a tooth structure is designed based on thin shell theory and the energy loss principle. Using a finite element simulation method combined with multivariate linear regression equations, the linear influence of each structural parameter on overall performance is investigated. A multi-objective optimization model using three key indices as objective functions is constructed and optimized with the NSGA-II algorithm, providing a set of optimization parameters for subsequent research. It establishes equivalent mathematical models for different forms of electrostatic forces and verify their validity using finite element simulations. Finally, the resonator’s response under different excitation forms is experimentally validated. Results show that the resonator exhibits optimal resonance under single-octave sinusoidal excitation: the four-wave belly oscillation pattern remains intact in driving mode with no frequency crosstalk. The resonant amplitude limit is 0.34 nm, significantly greater than under other excitation forms. The proposed method achieves comprehensive performance optimization of the metal resonator and provides a theoretical basis for selecting excitation forms in resonant gyros.

IEEE Transactions on Instrumentation and MeasurementVol. 74
National University of Singapore (SG), Chinese Academy of Sciences (CN), Aerospace Information Research Institute (CN), Beijing Information Science & Technology University (CN)
Natural Science Foundation of Beijing Municipality, National Key Research and Development Program of China
Openalex Percentile: Top 7%
Inertial Sensor and Navigation
4.99
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