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dc.contributor.authorChang, Cheng-Yangen_US
dc.contributor.authorChen, Tsung-Linen_US
dc.date.accessioned2017-04-21T06:50:03Z-
dc.date.available2017-04-21T06:50:03Z-
dc.date.issued2016en_US
dc.identifier.isbn978-1-4673-8829-0en_US
dc.identifier.urihttp://hdl.handle.net/11536/134382-
dc.description.abstractThis paper proposed a new design of the dual-axis control input, dual-axis position measurement piezoelectric gyroscope. Using piezoelectric actuation/sensing to implement this gyroscope can be much more difficult than the conventional gyroscope, which equips only single-axis control input and dual-axis position measurement. This is because multiple mode shapes may exist in the flexure deformation, which complicates the relation between flexure deformation and the proof mass position. This paper solves this multiple-mode-shape problem by designing the location and dimensions of the electrodes such that the piezoelectric force would not excite multiple mode shapes and the voltage output of the sensing electrodes responds only to specific mode shapes. The proposed design achieves a sensitivity of 8 mu v/deg/sec for the angular rate sensing and a quadrature error of 0.007%. The low quadrature error could be one of the advantages of sensing the position of the proof mass via sensing the specific deformed shape of the flexure.en_US
dc.language.isoen_USen_US
dc.subjectpiezoelectric gyroscopeen_US
dc.subjectpiezoelectric actuationen_US
dc.subjectpiezoelectric position sensingen_US
dc.subjectcross-axis couplingen_US
dc.subjectdual-axis control inputen_US
dc.subjectquadrature erroren_US
dc.titleDesign and Simulation of a New Dual-Axis Control Input Piezoelectric Gyroscopeen_US
dc.typeProceedings Paperen_US
dc.identifier.journalPROCEEDINGS OF 2016 7TH INTERNATIONAL CONFERENCE ON MECHANICAL AND AEROSPACE ENGINEERING, (ICMAE)en_US
dc.citation.spage274en_US
dc.citation.epage278en_US
dc.contributor.department機械工程學系zh_TW
dc.contributor.departmentDepartment of Mechanical Engineeringen_US
dc.identifier.wosnumberWOS:000390417000051en_US
dc.citation.woscount0en_US
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