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Vibration non-sensitive silicon micro-electromechanical gyroscope

A silicon micro-electromechanical gyro, non-sensitive technology, applied in the direction of gyro effect for speed measurement, gyroscope/steering sensing equipment, measuring device, etc., to achieve the effect of improving anti-vibration characteristics, high measurement accuracy, and reducing the volume of gyro

Active Publication Date: 2020-03-27
BEIJING INST OF AEROSPACE CONTROL DEVICES
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

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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  • Vibration non-sensitive silicon micro-electromechanical gyroscope
  • Vibration non-sensitive silicon micro-electromechanical gyroscope
  • Vibration non-sensitive silicon micro-electromechanical 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

The vibration non-sensitive silicon micro-electromechanical gyroscope comprises a four-mass tuning fork microstructure, a control circuit, a packaging shell and a shock absorber assembly, the four-mass tuning fork microstructure is a two-degree-of-freedom motion microstructure machined based on the SOG technology, and the four mass blocks move in the X direction and the Y direction in the plane under the stress condition. The control circuit is composed of a C / V conversion circuit, a drive shaft self-excitation loop, a detection shaft force balance loop, an MCU control circuit and the like. The micro structure and the control circuit board are packaged together by the packaging shell, and an external mechanical interface is formed through four mounting holes of the shell; and the shock absorber assembly is a connecting mechanism between the circuit board and the packaging shell. The high-precision vibration non-sensitive silicon micro-electro-mechanical gyroscope is high in measurementprecision and resistant to vibration impact, can be widely applied to systems such as guided bombs, portable air defense missiles, intelligent shells, unmanned aerial vehicles and navigation equipment, and is used for measuring the rotation angle rate of a carrier around a fixed shaft relative to an 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 Applications(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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