Three-Axis Gyroscope Structure for Orthogonal Mode Decoupling

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

Traditional three-axis gyroscopes suffer from mutual coupling errors in their X, Y, and Z axes, leading to large coupling errors and the inability to achieve electrical orthogonal suppression and capacitance modality matching simultaneously.

Innovation Solution

A three-axis gyroscope design with independent first, second, and third sensitive structures, each connected by elastic members, allowing for orthogonal detection modalities without interference, and incorporating drive structures with drive electrodes to facilitate differential motion and capacitance changes for accurate angular velocity measurement.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Measurement precision

If traditional three-axis gyroscope structure is used, then device complexity is reduced, but measurement precision deteriorates due to mutual coupling errors in X, Y, and Z axes

Engineering Contradiction:
Improveangular velocity measurement accuracyVSAvoidstructure complexity
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The gyroscope is divided into three independent sensitive structures (first, second, and third sensitive structures), each responsible for detecting angular velocity in a specific direction. Each sensitive structure includes its own mass blocks, elastic members, and drive portions, allowing independent operation and eliminating mutual coupling errors between axes while maintaining overall system functionality.

Inventive Principle:
Principle #1Segmentation

2Measurement precision

If electrical control of detection modality is applied to suppress coupling errors, then measurement precision improves, but device complexity increases due to additional control mechanisms

Engineering Contradiction:
Improvedetection accuracyVSAvoidcontrol system complexity
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The sensitive structures utilize their own inherent elastic members and mass blocks to generate and detect vibrations without requiring external electrical control mechanisms. The drive portions directly drive the mass blocks to vibrate in specific directions, and the detection is performed by measuring these vibrations, eliminating the need for complex electrical suppression systems.

Inventive Principle:
Principle #25Self-service

3Measurement precision

If capacitance modality matching is implemented, then measurement precision improves, but ease of manufacture deteriorates due to stricter manufacturing tolerances

Engineering Contradiction:
Improvecapacitance matching accuracyVSAvoidmanufacturing tolerance requirements
Core Design Contradiction:
Measurement precisionVSEase of manufacture

Solution Approach 1:

The elastic members are designed with specific local properties (flexibility, strength, and dimensional characteristics) that are optimized for their individual functions. By carefully designing the local geometry and material properties of each elastic member, the system achieves capacitance modality matching without requiring extremely tight overall manufacturing tolerances, as each component's local characteristics can be independently optimized.

Inventive Principle:
Principle #3Local quality

Applied Scientific Principles

This section explains which scientific principles are used to turn an abstract innovation direction into a practical engineering solution.

Function Achieved in This Case

The design achieves high detection sensitivity and accuracy by eliminating coupling errors, enabling electrical orthogonal suppression and capacitance modality matching, thereby improving the overall performance and stability of the gyroscope.

Implementation Method 1

first elastic members for connecting the first sensitive structure and the drive structure; the three-axis gyroscope comprises fourth elastic members, the first drive portions and the third drive portions are respectively connected to two end portions of the drive arms along the first direction through the fourth elastic members

Methodology Applied
Scientific EffectElastic deformation: Elasticity

Implementation Method 2

the drive structure comprises first drive portions, drive arms, and third drive portions, and second drive portions are formed on the drive arms; the drive structure further comprises drive electrodes which are mounted on the first drive portions and the third drive portions

Methodology Applied
Scientific EffectElectrostatic force: Electrostatics

Implementation Method 3

the first drive portions are connected with the first sensitive structure through the first elastic members; the first mass block and the second mass block can move towards or away from each other in the second direction

Methodology Applied
Scientific EffectCapacitance change: Capacitance

Implementation Method 4

A micro-electromechanical system (MEMS) gyroscope in the prior art can detect an angular velocity according to the generation principle of Coriolis force

Methodology Applied
Scientific EffectCoriolis force: Coriolis Force

Data Source

PatentUS20260015223A1Three-axis gyroscope
Publication Date: 2026.01.15 AAC KAITAI TECHNOLOGIES (WUHAN) CO LTD
  • US20260015223A1 patent drawing
  • US20260015223A1 patent drawing
  • US20260015223A1 patent drawing

AI summary

The present invention provides a three-axis gyroscope and electronic products, including a drive structure used for driving the three-axis gyroscope, a first sensitive structure used for sensing an angular velocity in a first direction, a second sensitive structure used for sensing an angular velocity in the second direction, a third sensitive structure used for sensing an angular velocity in a third direction. The first sensitive structure, the second sensitive structure and the third sensitive structure can be mutually coupled in the first detection modality, the second detection modality and the third detection modality, which can effectively avoid the coupling error, achieve electrical orthogonal suppression and capacitance modality matching in the first detection modality, the second detection modality or the third detection modality, so that the structural performance loss can be compensated, thus reducing an orthogonal error and improving the detection accuracy and overall performance of the three-axis gyroscope.