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Influence of Zero Output State of Quartz Gyroscope under Active Vibration of Pneumatic-servo-actuator

  • LIU Kui 1 ,
  • JIANG Junbiao 1 ,
  • GOU Zhiping 2 ,
  • LIU Lida 3
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  • 1 Xi’an Modern Control Technology Research Institute,Xi’an 710065,China
  • 2 No.26 China Electronics Technology Group Corporation,Chongqing 400060,China
  • 3 Henan North Hong-yang Electromechanical Co., Ltd.,Nanyang 473000,Henan,China

Received date: 2022-02-10

  Online published: 2025-02-03

Abstract

Quartz gyroscope is a typical vibrating gyroscope. Its zero position control technology indifferent carrier vibration environment is very important for the accurate measurement of guided weapon’s attitude. Because the quartz gyroscope has some basic physical parameters, such as driving frequency, resonance frequency and frequency difference, it is inevitable that the fundamental frequency and octave frequency of the carrier may overlap and interfere with each other. This paper analyzes the interaction of driving frequency, detection frequency, carrier fundamental frequency and octave frequency as well as their influence forms on the zero position output state of the gyroscope, designs the optimization scheme of driving frequency of different carrier frequencies of the quartz gyroscope, and carriers out vibration test verification.The test results show that under the condition of carrier fundamental frequency, the driving frequency of quartz gyroscope can effectively control the output state of gyro zero position.

Cite this article

LIU Kui , JIANG Junbiao , GOU Zhiping , LIU Lida . Influence of Zero Output State of Quartz Gyroscope under Active Vibration of Pneumatic-servo-actuator[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2022 , 42(3) : 110 -115 . DOI: 10.15892/j.cnki.djzdxb.2022.03.021

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[1]
YING W, YUNAN S, BINGKUN Q, et al. Study on the modal characteristics of quartz tuning fork angular rate microsensor by means of FEM[C]// SPIE. Proceedings of the 2000 Conference on Process Control and Inspection for Industry. Washington: SPIE, 2000: 87-90.

[2]
王莹, 孙雨南, 秦秉坤, 等. 微石英音叉陀螺激励与检测电极的研究[J]. 北京理工大学学报(自然科学版), 2001, 21(4):503-507.

[3]
廖兴才. 微型石英音又陀螺结构设计与信号处理[D]. 北京: 北京理工大学, 2004.

[4]
HAO Z L, ERBIL A, AYAZI F. An analytical model for support loss in micromachined beam resonators with in-plane flexural vibrations[J]. Sensors and Actuators, 2003, 109(1/2): 156-164.

[5]
张正福. 音叉振动式微机械陀螺结构动态性能解析与健壮性设计[D]. 上海: 上海交通大学机械与动力工程学院, 2007.

[6]
林日乐, 谢佳维, 周倩, 等. 石英MEMS陀螺的结构特性分析[J]. 压电与声光, 2011, 33(4):544-546.

[7]
施芹, 裘安萍, 苏岩, 等. 硅微陀螺仪的机械耦合误差分析[J]. 光学精密工程, 2008, 19(5):894-898.

[8]
林日乐, 谢佳维, 王伟, 等. 石英微机电陀螺的频率干扰特性研究[J]. 压电与声光, 2020, 42(2):186-188.

[9]
白冰, 赵玉龙. 微型石英音叉谐振陀螺抗冲击的建模与仿真[J]. 导航与控制, 2019, 18(4):25-32.

DOI

[10]
李宇鹏, 王志飞, 刘来超. 音叉式全解耦微机电陀螺的设计与仿真[J]. 机械设计, 2016, 33(8):33-37.

[11]
冯立辉, 俞建国, 崔芳, 等. 微石英音叉陀螺仪信号检测研究[J]. 仪器仪表学报, 2006, 27(6):41-46.

Outlines

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