Microring gyroscopes are promising candidates for inertial navigation systems due to their exceptional performance, robustness in harsh environments, and relatively low cost, which makes them well suited for applications such as self-driving car navigation systems. Previous models of ring gyroscopes often relied on the assumed mode method and low-order multi-elements finite element analysis (FEA) to predict gyroscope performance, while simplifying the geometry for ease of computation. In this paper, a modeling approach that uses higher-order curved beam finite elements is proposed. This approach leads to a clear relation between the gyroscope’s dynamic performance and its geometric parameters. Consequently, this approach allows the gyroscope designer to decide the performance of the gyroscope by using one geometric parameter and it leaves a room for him to select material properties and other dimensions based on other design considerations. The dynamic performance is measured by the scale factor, which is directly proportional to the Coriolis constant. The proposed approach is validated by comparing its results with finite element simulation software, demonstrating an estimation error of less than 5% over a specific design range. The proposed method not only improves the accuracy of gyroscope modeling but also offers a straightforward approach to modeling more complex gyroscopes, such as multi-ring gyroscopes, without significantly increasing formulation complexity.
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