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High-precision horizontal-axis silicon micro-gyroscope based on tuning fork driving effect

A silicon micro-gyroscope, high-precision technology, applied in the direction of the gyro effect for speed measurement, gyroscope/steering sensing equipment, instruments, etc., can solve the problem of high coupling degree of monolithic integrated three-axis gyroscope, which is not conducive to the miniaturization of micro-inertial system , limit the development and application of micro-inertial devices, etc., to achieve the effect of improving detection sensitivity, improving structural quality factor, and high sensitivity of detection capacitance

Active Publication Date: 2020-10-16
BEIJING INST OF AEROSPACE CONTROL DEVICES
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Problems solved by technology

This placement leads to an increase in the volume of the inertial measurement unit, which is not conducive to the miniaturization of the micro-inertial system
However, there is still a big gap between the accuracy and integration of domestic single-chip integrated three-axis gyroscopes compared with foreign advanced technologies, which greatly limits the development and application of domestic micro-inertial devices. The coupling degree of the direction is high, which is not conducive to high-precision measurement

Method used

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  • High-precision horizontal-axis silicon micro-gyroscope based on tuning fork driving effect
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  • High-precision horizontal-axis silicon micro-gyroscope based on tuning fork driving effect

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Embodiment Construction

[0025] Exemplary embodiments of the present disclosure will be described in more detail below with reference to the accompanying drawings. Although exemplary embodiments of the present disclosure are shown in the drawings, it should be understood that the present disclosure may be embodied in various forms and should not be limited by the embodiments set forth herein. Rather, these embodiments are provided for more thorough understanding of the present disclosure and to fully convey the scope of the present disclosure to those skilled in the art. It should be noted that, in the case of no conflict, the embodiments of the present invention and the features in the embodiments can be combined with each other. The present invention will be described in detail below with reference to the accompanying drawings and examples.

[0026] figure 1 It is a schematic structural diagram of a high-precision horizontal-axis silicon micro-gyroscope based on a tuning fork driving effect provided...

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Abstract

The invention discloses a high-precision horizontal-axis silicon micro-gyroscope based on a tuning fork driving effect. The high-precision horizontal-axis silicon micro-gyroscope comprises a cap layer, a gyroscope sensitive structure and a substrate layer, wherein the cap layer and the substrate layer are connected to form an internal vacuum structure, and the gyroscope sensitive structure is arranged in the internal vacuum structure; the gyroscope sensitive structure comprises a first driving comb tooth group, a second driving comb tooth group, a third driving comb tooth group, a fourth driving comb tooth group, a first driving detection comb tooth, a second driving detection comb tooth, a third driving detection comb tooth, a fourth driving detection comb tooth, a first driving elastic beam group, a second driving elastic beam group, a first detection elastic beam group, a second detection elastic beam group, an anchor area group, a first mass block, a second mass block, a coupling elastic beam, a first driving frame and a second driving frame. According to the invention, measurement of pitching and rolling angular rates is realized, and the size of an inertial measurement unit is reduced.

Description

technical field [0001] The invention belongs to the technical field of micro-mechanical inertial instruments, and in particular relates to a high-precision horizontal-axis silicon micro-gyroscope based on the tuning fork driving effect, which can be applied to systems such as guided bombs, portable anti-aircraft missiles, mobile devices, unmanned aerial vehicles, and navigation equipment. It is used to measure the angular rate of rotation of the carrier around a fixed axis relative to the inertial space. Background technique [0002] The gyroscope is a sensor that measures the rotational motion of the carrier relative to the inertial space. It is the core device in the fields of motion measurement, inertial navigation, guidance and control, etc. It is very important in high-end industrial equipment and precision strike weapons such as aerospace, unmanned driving, and guided munitions. application value. With the continuous development of application fields such as individua...

Claims

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Application Information

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IPC IPC(8): G01C19/5621G01C19/5614G01C19/5726G01C19/5733G01C19/56
CPCG01P9/04G01C19/5621G01C19/5614G01C19/5726G01C19/5733
Inventor 刘国文高乃坤徐杰张乐民王健鹏刘福民
Owner BEIJING INST OF AEROSPACE CONTROL DEVICES
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