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Conference Paper: Application of inerter to aircraft landing gear suspension

TitleApplication of inerter to aircraft landing gear suspension
Authors
KeywordsAircraft landing gear
Inerter
Shimmy vibration
Suspension
Issue Date2015
PublisherInstitute of Electrical and Electronics Engineers. The Journal's web site is located at http://www.ieeexplore.ieee.org/xpl/conhome.jsp?punumber=1001331
Citation
The 34th Chinese Control Conference (CCC 2015), Hangzhou, China, 28-30 July 2015. In Chinese Control Conference, 2015, p. 2066-2071 How to Cite?
AbstractThe inerter was recently proposed as a two-terminal mechanical element with the property that the force across the element is proportional to the relative acceleration of its two terminals. Improvement has been observed through introducing inerters into various suspension systems. In this paper, the investigation is focused on the shimmy vibration in the aircraft landing gears and the performance variation with the application of inerters. By the method of simulation, the performance changes have been observed and analyzed.
DescriptionOpen Access
Persistent Identifierhttp://hdl.handle.net/10722/217418
ISSN

 

DC FieldValueLanguage
dc.contributor.authorDong, X-
dc.contributor.authorLiu, Y-
dc.contributor.authorChen, MZ-
dc.date.accessioned2015-09-18T05:58:56Z-
dc.date.available2015-09-18T05:58:56Z-
dc.date.issued2015-
dc.identifier.citationThe 34th Chinese Control Conference (CCC 2015), Hangzhou, China, 28-30 July 2015. In Chinese Control Conference, 2015, p. 2066-2071-
dc.identifier.issn1934-1768-
dc.identifier.urihttp://hdl.handle.net/10722/217418-
dc.descriptionOpen Access-
dc.description.abstractThe inerter was recently proposed as a two-terminal mechanical element with the property that the force across the element is proportional to the relative acceleration of its two terminals. Improvement has been observed through introducing inerters into various suspension systems. In this paper, the investigation is focused on the shimmy vibration in the aircraft landing gears and the performance variation with the application of inerters. By the method of simulation, the performance changes have been observed and analyzed.-
dc.languageeng-
dc.publisherInstitute of Electrical and Electronics Engineers. The Journal's web site is located at http://www.ieeexplore.ieee.org/xpl/conhome.jsp?punumber=1001331-
dc.relation.ispartofChinese Control Conference-
dc.rightsChinese Control Conference. Copyright © Institute of Electrical and Electronics Engineers.-
dc.rights©2015 IEEE. Personal use of this material is permitted. Permission from IEEE must be obtained for all other uses, in any current or future media, including reprinting/republishing this material for advertising or promotional purposes, creating new collective works, for resale or redistribution to servers or lists, or reuse of any copyrighted component of this work in other works.-
dc.subjectAircraft landing gear-
dc.subjectInerter-
dc.subjectShimmy vibration-
dc.subjectSuspension-
dc.titleApplication of inerter to aircraft landing gear suspension-
dc.typeConference_Paper-
dc.identifier.emailChen, MZ: mzqchen@hku.hk-
dc.identifier.authorityChen, MZ=rp01317-
dc.description.naturelink_to_OA_fulltext-
dc.identifier.doi10.1109/ChiCC.2015.7259953-
dc.identifier.hkuros250978-
dc.identifier.spage2066-
dc.identifier.epage2071-
dc.publisher.placeUnited States-
dc.customcontrol.immutablesml 151109-

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