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A Closed-Loop Method of Angular Rate for Improving Mems Gyroscope's Static and Linear Index

A closed-loop method and angular rate technology, applied in electrostatic sensors, semiconductor electrostatic transducers, sensors, etc., can solve problems such as being difficult to meet, and achieve the advantages of small external influence factors, improved dynamic response speed, and good signal-to-noise ratio advantages. Effect

Active Publication Date: 2020-09-22
XIAN FLIGHT SELF CONTROL INST OF AVIC
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Its basic principle is based on the Coriolis effect of mechanical resonance, which is essentially a kind of mechanical resonance gyroscope. High-precision MEMS gyroscopes have been successfully used in many occasions and environments, but the contradiction between static high precision and bandwidth of MEMS gyroscopes The problem is difficult to deal with, although the static performance of the MEMS gyroscope has reached the rate level (10-1000( ○ ) / h), but in terms of dynamic range, it is difficult to meet the requirements of bandwidth >70Hz (rate level), because high-precision MEMS gyroscopes often need to reduce the difference Δf between the driving and detection mode natural frequencies to obtain a higher High mechanical gain, and the mechanical bandwidth of the MEMS gyro open-loop detection direction is about half of Δf. Therefore, in order to obtain high mechanical gain, the high-precision MEMS gyroscope needs to sacrifice the bandwidth index of the MEMS gyroscope. The angular rate closed-loop is used in the detection mode. The method can effectively solve the contradiction between the static accuracy and bandwidth of the MEMS gyroscope

Method used

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  • A Closed-Loop Method of Angular Rate for Improving Mems Gyroscope's Static and Linear Index
  • A Closed-Loop Method of Angular Rate for Improving Mems Gyroscope's Static and Linear Index
  • A Closed-Loop Method of Angular Rate for Improving Mems Gyroscope's Static and Linear Index

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Effect test

Embodiment 1

[0046] After adding the angular rate closed-loop function to the MEMS gyroscope, the mechanical non-orthogonal error term of the MEMS gyroscope can remain stable under the full temperature environment, and the angular rate error input of the MEMS gyroscope is also maintained at a stable zero input position, that is, the angular rate closed-loop The advanced MEMS gyroscope can approach the error term of the gyroscope's detection mode to zero, so that the MEMS gyroscope is in a balanced position in the detection mode.

[0047] When the angular rate error term of the MEMS gyroscope is zero, the mechanical non-orthogonal error term of the MEMS gyroscope also tends to zero, the scale factor coefficient of the MEMS gyroscope is reduced by the influence of the external environment, and the gyroscope does not exist in the external environment. The non-orthogonal error term greatly enhances the stability of the scale factor of the gyroscope. The MEMS gyroscope with the angular rate clos...

Embodiment 2

[0050] The static index and dynamic bandwidth of the MEMS gyroscope are a pair of contradictory communities. After adding the angular rate closed-loop function to MEMS gyroscope products, the MEMS gyroscope can effectively increase the bandwidth of the gyroscope while increasing the static gain, breaking through the contradiction between bandwidth and static accuracy, and improving the zero bias stability test performance of the MEMS gyroscope. An order of magnitude, the static bias stability index of the MEMS gyroscope has been improved by an order of magnitude, and can meet the requirements of 5 ○ The tactical-level use requirements of / h make the application of MEMS gyroscopes more ideal in attitude control, measurement systems, positioning and orientation, and make MEMS gyroscopes fully reflect the application advantages of MEMS gyroscopes in the fields of downhole trajectory measurement and track trajectory measurement.

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Abstract

The invention discloses an angular rate closed-loop method for improving the static and linearity indexes of a MEMS gyro, belonging to the sensor control field. The invention optimizes the control mode of an angular rate closed loop MEMS gyro, and adopts a fourth-order sigma-Delta feedforward sum circuit detects that modal displacement error signal detect by gyro, uses comb electrode to feedback control angular rate error information, parallel plate electrode to correct mechanical non-orthogonal error signal, angle rate error channel adopts direct-I type control, mechanical non-orthogonal error signal adopts direct-I type control, and mechanical non-orthogonal error signal adopts direct-I type control. Type II controller, so that the sensing mode of the MEMS gyro is always under the condition of zero rotational speed input, Finally, the closed-loop control is formed by superposing the closed-loop control signals, the MEMS gyroscope always keeps the balance position in the detection mode, and the MEMS gyroscope controlled by the servo system always works at a specific working point, so the static performance and dynamic performance of the MEMS gyroscope are improved.

Description

technical field [0001] The invention discloses an angular rate closed-loop method for improving the static and linearity indexes of MEMS gyroscopes, belonging to the technical field of sensor control. Background technique [0002] MEMS gyroscope is a new type of angular rate sensor. Its basic principle is based on the Coriolis force effect of mechanical resonance, which is essentially a kind of mechanical resonance gyroscope. High-precision MEMS gyroscopes have been successfully used in many occasions and environments, but the contradiction between static high precision and bandwidth of MEMS gyroscopes The problem is difficult to deal with, although the static performance of the MEMS gyroscope has reached the rate level (10-1000( ○ ) / h), but in terms of dynamic range, it is difficult to meet the requirements of bandwidth >70Hz (rate level), because high-precision MEMS gyroscopes often need to reduce the difference Δf between the driving and detection mode natural frequen...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): H04R19/00
CPCH04R19/005H04R2201/003
Inventor 孟冰吕航伟王刚李文宏
Owner XIAN FLIGHT SELF CONTROL INST OF AVIC
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