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A vibration-insensitive silicon MEMS gyroscope

A silicon micro-electromechanical gyroscope, non-sensitive technology, applied in the direction of speed measurement, gyroscope/steering sensing equipment, instruments, etc., to achieve the effect of reducing measurement error, improving anti-vibration characteristics, and reducing the size of the gyroscope

Active Publication Date: 2021-12-07
BEIJING INST OF AEROSPACE CONTROL DEVICES
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Problems solved by technology

[0004] The technical problem of the present invention is: through the method of combining the fully symmetrical and fully differential four-mass double-tuning fork micro-sensitive structure and the external shock absorber assembly, the high-precision capacitance signal detection and control technology is used to realize the complex vibration of the silicon micro-electromechanical gyroscope. High accuracy of angular rate measurement can be maintained under mechanical environment

Method used

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  • A vibration-insensitive silicon MEMS gyroscope
  • A vibration-insensitive silicon MEMS gyroscope
  • A vibration-insensitive silicon MEMS gyroscope

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Embodiment Construction

[0038] The present invention proposes a high-precision vibration-insensitive silicon micro-electromechanical gyroscope based on a four-mass double-tuning fork micro-sensitive structure. The axial direction of the sensitive input angular rate is the Z direction, and its structure includes a four-mass double-tuning fork microstructure, a control circuit, and a packaging shell. Body and shock absorber components. The control circuit and the microstructure of the four-mass double-tuning fork are welded on a circuit board and installed in the metal package shell through the shock absorber assembly, and the digital output signal proportional to the input angular rate is drawn out through the wire.

[0039] Such as figure 1 Shown is the principle block diagram of the high-precision vibration non-sensitive silicon micro-electromechanical gyroscope of the present invention, which includes a four-mass double-tuning fork micro-sensitive structure and a control circuit. The control circui...

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Abstract

A vibration-insensitive silicon micro-electromechanical gyroscope, including a four-mass tuning fork microstructure, a control circuit, a packaging case and a shock absorber assembly; the four-mass tuning fork microstructure is a two-degree-of-freedom motion microstructure processed based on SOG technology, and four The mass block moves along the X and Y directions in the plane under the condition of force; the control circuit is composed of C / V conversion circuit, drive shaft self-excitation circuit, detection axial force balance circuit, MCU control circuit, etc.; the package shell combines the microstructure and The control circuit board is packaged together and forms an external mechanical interface through four mounting holes of the housing; the shock absorber assembly is the connection mechanism between the circuit board and the packaging housing. The invention is a high-precision vibration non-sensitive silicon micro-electromechanical gyroscope, which has high measurement accuracy and anti-vibration impact, and can be widely used in systems such as guided bombs, portable anti-aircraft missiles, intelligent shells, unmanned aerial vehicles, navigation equipment, etc., for measuring carriers The angular rate of rotation about a fixed axis relative to inertial space.

Description

technical field [0001] The invention relates to a high-precision vibration non-sensitive silicon micro-electromechanical gyro based on a four-mass double-tuning fork micro-sensitive structure, which belongs to the field of micro-mechanical inertial instruments and can be applied to guided bombs, portable anti-aircraft missiles, intelligent shells, unmanned aerial vehicles, and navigation equipment. and other systems for measuring the angular rate of rotation of a carrier around a fixed axis relative to inertial space. Background technique [0002] Silicon micro-electromechanical gyroscope is a new type of micro-mechanical inertial instrument developed in the 1980s. It belongs to the category of micro-electro-mechanical systems. It is generally composed of micro- or nano-scale movable micro-structures and control circuits for sensitive micro-signals. The angular rate of rotation about a fixed axis relative to inertial space. It is manufactured using micro-electromechanical p...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G01C19/5621G01C19/5614G01C19/5628
CPCG01C19/5614G01C19/5621G01C19/5628
Inventor 徐杰刘福民李兆涵高乃坤赵亭杰王建鹏刘国文杨静张乐民
Owner BEIJING INST OF AEROSPACE CONTROL DEVICES
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