MEMS gyroscope is widely used in various fields because of its advantages of low power consumption, light weight and low cost. High-precision MEMS gyro can improve the attitude measurement and control accuracy of many types of equipment and platforms, and is expected to solve the autonomous navigation problem of unmanned vehicles, drones and other equipment in complex environments, and has broad development prospects, so it is always one of the hot research directions in the field of inertia. The evolution of resonant structure of high precision MEMS gyro is described in this paper. The mass-block MEMS gyro and rotator-symmetric MEMS gyro are introduced.



Mass block MEMS gyroscope


1. Single-mass MEMS gyroscope

Based on the basic mass-spring dynamics model of MEMS gyro, it can be roughly divided into centralized mass block structure and distributed mass structure. The single mass mass structure is supported by the elastic structure, which is the most intuitive manifestation of the basic dynamic model. It is usually designed as a decoupled structure, such as the typical universal-joint micro-vibration structure, where a mass block is supported by two nested outer frames that can be twisted. As shown in Figure 1, when the gyro is working, the central mass block torsional vibrates along a fixed direction with a certain amplitude and frequency; When there is an angular velocity input, the Coriolis force will also vibrate in the other direction, and the amplitude of the vibration is proportional to the angular velocity input.

The gyro sensitivity can be improved by adjusting the structural parameters to increase the vibration displacement.



Figure 1 Typical MEMS gyro structure



2. Dual mass MEMS gyroscope

On the basis of the single-mass mass block structure, the resonant structure is designed as a mass block with two symmetrical modes, then a double-mass MEMS gyro sensor (also known as tuning fork gyroscope) is formed. The typical structure is shown in Figure 2. This design can solve the problem of center of mass deflection caused by structural vibration, effectively reduce the support loss, and make MEMS gyro have the potential of medium and high precision. Honeywell's latest report on the tuning fork type micro-electromechanical gyroscope zero-bias instability (the following are Allan variance) is 0.02°/h, the range is greater than 990°/s, and the scaling factor nonlinear is 13 ppm. The bias instability of the comb electrode structure gyroscope developed by Tronics company in France is 0.8°/h, the range is ±300°/s, and the scale factor nonlinearity is 230 ppm.



Figure 2 Typical high-precision dual-mass MEMS gyro structure



3. Four-mass MEMS gyro

In order to further increase the symmetry of mass block distribution, four-mass MEMS gyro has been further evolved on the basis of two-mass MEMS gyro, which is generally composed of four symmetrically distributed mass blocks connected through a beam structure, and its inertial mass and quality factor are further improved, so it has better sensitivity and mechanical thermal noise level.

Because of the symmetry of the structure, the four-mass MEMS gyro can work in frequency matching mode to improve the detection sensitivity. Asadian et al., University of California, Irvine, designed a four-mass MEMS gyro based on the inverse relative symmetric operating mode. The fulcrum is in force balance during operation, so the support loss is very small. At the same time, the thermoelastic damping of the structure can be reduced by reducing the resonant frequency and wall thickness, and the quality factor can be close to 2×106. In rate integration mode, the zero bias instability of the gyroscope is 0.2°/h, the Angle random travel is 0.02°/h1/2, and the range can exceed 1000°/s. In the force feedback mode, the angular random walk is 0.015°/h1/2, and the zero-bias instability is 0.09°/h. Tsinghua University designed a four-mass MEMS gyro supported by a cross beam (FIG. 3). The adjacent mass blocks are connected to each other by a bent flexible beam. The working detection modes are symmetrical, and the Q value is 16000. The zero-bias instability is 0.12°/h and the angular random walk is 0.012°/h1/2.



Figure 3 Typical four-mass MEMS gyro structure and operating modes



The four-mass MEMS gyro can also work in the asymmetric drive detection mode, which also shows better performance. Sensonor has developed a sphenowing microelectromechanical gyroscope based on the four-mass resonant structure of the IMEGO Institute, as shown in Figure 4(a). Its latest STIM300 series products have a measuring range of ±400°/s, zero bias instability of 0.5°/h at room temperature, and good zero bias temperature sensitivity (0.08°/h/°C) and scale factor nonlinear (15 ppm). National University of Defense Technology has optimized the sensitive structure of the spidey-wing silicon micro gyro, as shown in Figure 4(b). The machining error is effectively reduced by the full pre-burial process, and the precise machining of the silicon inclined beam is realized. At the same time, the thermal stress deformation and packaging stress in gyro machining are effectively reduced by stress release and equilibrium structure. The zero bias instability is 0.19°/h, the scale range is ±200°/s, and the scale factor nonlinearity is 89.6 ppm.



Figure. 4 Structure of sphenowing microelectromechanical gyroscope



Conclusion


This paper focuses on the structure evolution of high-precision MEMS gyro. In terms of the resonant structure evolution of high-precision MEMS gyro, two-mass, four-mass, ring MEMS gyro and micro-hemispherical resonator gyro have been reported to have better performance, some products have been better than the tactical level accuracy index, and a few have been close to the navigation level accuracy threshold. With the application of topology optimization design, new materials and new processes, the structural innovation of MEMS gyro is still worth looking forward to. At the same time, we can pay attention to the ER-MG-067 tactical MEMS gyroscope, which uses a single mass block structure, its zero bias stability can reach 3°/hr, and the angular velocity random walk is 0.125°/√hr. In high-precision fields such as drones, navigation grade MEMS gyroscope is needed, such as ER-MG2-50/100, whose zero-bias instability can reach 0.01-0.02°/hr, and angular velocity random walk can reach 0.0025-0.005°/√hr.

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