Enhanced sensitivity in a butterfly gyroscope with a hexagonal oblique beam

A new approach to improve the performance of a butterfly gyroscope is developed. The methodology provides a simple way to improve the gyroscope’s sensitivity and stability, by reducing the resonant frequency mismatch between the drive and sense modes. This method was verified by simulations and theo...

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Main Authors: Dingbang Xiao, Shijie Cao, Zhanqiang Hou, Zhihua Chen, Xinghua Wang, Xuezhong Wu
Format: Article
Language:English
Published: AIP Publishing LLC 2015-04-01
Series:AIP Advances
Online Access:http://dx.doi.org/10.1063/1.4916587
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spelling doaj-93675db04b564ae3b27c151bf6c7e5102020-11-24T21:08:09ZengAIP Publishing LLCAIP Advances2158-32262015-04-0154041331041331-810.1063/1.4916587029593ADVEnhanced sensitivity in a butterfly gyroscope with a hexagonal oblique beamDingbang Xiao0Shijie Cao1Zhanqiang Hou2Zhihua Chen3Xinghua Wang4Xuezhong Wu5College of Mechatronics Engineering and Automation, National University of Defense Technology, Changsha, Hunan, 410073, ChinaCollege of Mechatronics Engineering and Automation, National University of Defense Technology, Changsha, Hunan, 410073, ChinaCollege of Mechatronics Engineering and Automation, National University of Defense Technology, Changsha, Hunan, 410073, ChinaCollege of Mechatronics Engineering and Automation, National University of Defense Technology, Changsha, Hunan, 410073, ChinaCollege of Mechatronics Engineering and Automation, National University of Defense Technology, Changsha, Hunan, 410073, ChinaCollege of Mechatronics Engineering and Automation, National University of Defense Technology, Changsha, Hunan, 410073, ChinaA new approach to improve the performance of a butterfly gyroscope is developed. The methodology provides a simple way to improve the gyroscope’s sensitivity and stability, by reducing the resonant frequency mismatch between the drive and sense modes. This method was verified by simulations and theoretical analysis. The size of the hexagonal section oblique beam is the major factor that influences the resonant frequency mismatch. A prototype, which has the appropriately sized oblique beam, was fabricated using precise, time-controlled multilayer pre-buried masks. The performance of this prototype was compared with a non-tuned gyroscope. The scale factor of the prototype reaches 30.13 mV/ ˚/s, which is 15 times larger than that obtained from the non-tuned gyroscope. The bias stability of the prototype is 0.8 ˚/h, which is better than the 5.2 ˚/h of the non-tuned devices.http://dx.doi.org/10.1063/1.4916587
collection DOAJ
language English
format Article
sources DOAJ
author Dingbang Xiao
Shijie Cao
Zhanqiang Hou
Zhihua Chen
Xinghua Wang
Xuezhong Wu
spellingShingle Dingbang Xiao
Shijie Cao
Zhanqiang Hou
Zhihua Chen
Xinghua Wang
Xuezhong Wu
Enhanced sensitivity in a butterfly gyroscope with a hexagonal oblique beam
AIP Advances
author_facet Dingbang Xiao
Shijie Cao
Zhanqiang Hou
Zhihua Chen
Xinghua Wang
Xuezhong Wu
author_sort Dingbang Xiao
title Enhanced sensitivity in a butterfly gyroscope with a hexagonal oblique beam
title_short Enhanced sensitivity in a butterfly gyroscope with a hexagonal oblique beam
title_full Enhanced sensitivity in a butterfly gyroscope with a hexagonal oblique beam
title_fullStr Enhanced sensitivity in a butterfly gyroscope with a hexagonal oblique beam
title_full_unstemmed Enhanced sensitivity in a butterfly gyroscope with a hexagonal oblique beam
title_sort enhanced sensitivity in a butterfly gyroscope with a hexagonal oblique beam
publisher AIP Publishing LLC
series AIP Advances
issn 2158-3226
publishDate 2015-04-01
description A new approach to improve the performance of a butterfly gyroscope is developed. The methodology provides a simple way to improve the gyroscope’s sensitivity and stability, by reducing the resonant frequency mismatch between the drive and sense modes. This method was verified by simulations and theoretical analysis. The size of the hexagonal section oblique beam is the major factor that influences the resonant frequency mismatch. A prototype, which has the appropriately sized oblique beam, was fabricated using precise, time-controlled multilayer pre-buried masks. The performance of this prototype was compared with a non-tuned gyroscope. The scale factor of the prototype reaches 30.13 mV/ ˚/s, which is 15 times larger than that obtained from the non-tuned gyroscope. The bias stability of the prototype is 0.8 ˚/h, which is better than the 5.2 ˚/h of the non-tuned devices.
url http://dx.doi.org/10.1063/1.4916587
work_keys_str_mv AT dingbangxiao enhancedsensitivityinabutterflygyroscopewithahexagonalobliquebeam
AT shijiecao enhancedsensitivityinabutterflygyroscopewithahexagonalobliquebeam
AT zhanqianghou enhancedsensitivityinabutterflygyroscopewithahexagonalobliquebeam
AT zhihuachen enhancedsensitivityinabutterflygyroscopewithahexagonalobliquebeam
AT xinghuawang enhancedsensitivityinabutterflygyroscopewithahexagonalobliquebeam
AT xuezhongwu enhancedsensitivityinabutterflygyroscopewithahexagonalobliquebeam
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