Optimization of flexible multibody dynamic systems using the equivalent static load method
DC Field | Value | Language |
---|---|---|
dc.contributor.author | Kang, Byung-soo | - |
dc.contributor.author | Park, Gyung Jin | - |
dc.contributor.author | Arora, Jasbir Singh | - |
dc.date.accessioned | 2021-06-24T00:08:54Z | - |
dc.date.available | 2021-06-24T00:08:54Z | - |
dc.date.issued | 2005-04 | - |
dc.identifier.issn | 0001-1452 | - |
dc.identifier.issn | 1533-385X | - |
dc.identifier.uri | https://scholarworks.bwise.kr/erica/handle/2021.sw.erica/46480 | - |
dc.description.abstract | Recently, an algorithm for dynamic response optimization transforming dynamic loads into equivalent static loads has been proposed. In later research, it was proved that the solution obtained by the algorithm satisfies the Karush-Kuhn-Tucker necessary conditions. In the present research, the proposed algorithm is applied to the optimization of flexible multibody dynamic systems. The equivalent static load is derived from the equations of motion for a flexible multibody dynamic system. The equivalent load is utilized in sequential static response optimization of the flexible mutibody dynamic system. In the end, the converged solution of the sequential static response optimization is the solution of the original dynamic response optimization. Some standard examples are solved to show the feasibility and efficiency of the proposed method. The control arm of an automobile suspension system is optimized as a practical problem. The results are discussed regarding the application of the proposed algorithm to flexible multibody dynamic systems. Copyright © 2004 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved. | - |
dc.format.extent | 7 | - |
dc.language | 영어 | - |
dc.language.iso | ENG | - |
dc.publisher | American Institute of Aeronautics and Astronautics Inc. | - |
dc.title | Optimization of flexible multibody dynamic systems using the equivalent static load method | - |
dc.type | Article | - |
dc.publisher.location | 미국 | - |
dc.identifier.doi | 10.2514/1.4294 | - |
dc.identifier.scopusid | 2-s2.0-18144365511 | - |
dc.identifier.wosid | 000228246900015 | - |
dc.identifier.bibliographicCitation | AIAA Journal, v.43, no.4, pp 846 - 852 | - |
dc.citation.title | AIAA Journal | - |
dc.citation.volume | 43 | - |
dc.citation.number | 4 | - |
dc.citation.startPage | 846 | - |
dc.citation.endPage | 852 | - |
dc.type.docType | Article | - |
dc.description.isOpenAccess | N | - |
dc.description.journalRegisteredClass | scie | - |
dc.description.journalRegisteredClass | scopus | - |
dc.relation.journalResearchArea | Engineering | - |
dc.relation.journalWebOfScienceCategory | Engineering, Aerospace | - |
dc.subject.keywordPlus | OPTIMUM DESI | - |
dc.subject.keywordPlus | GNGENERAL-METHOD | - |
dc.subject.keywordPlus | BEHAVIOR | - |
dc.identifier.url | https://arc.aiaa.org/doi/10.2514/1.4294 | - |
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