Systematic design of tape spring hinges for solar array by optimization method considering deployment performances

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dc.contributor.authorKim, Kyung Wonko
dc.contributor.authorPark, Youngjinko
dc.date.accessioned2016-04-20T06:17:52Z-
dc.date.available2016-04-20T06:17:52Z-
dc.date.created2015-11-30-
dc.date.created2015-11-30-
dc.date.issued2015-10-
dc.identifier.citationAEROSPACE SCIENCE AND TECHNOLOGY, v.46, pp.124 - 136-
dc.identifier.issn1270-9638-
dc.identifier.urihttp://hdl.handle.net/10203/205238-
dc.description.abstractThis paper reports the systematic development of tape spring hinges for a solar array by an optimization method considering various deployment performances. The nonlinear behavior between the moment and the rotation angle of a tape spring hinge is determined through experimental results rather than through finite element analysis results or theoretical solutions in order to identify the moment-rotation profile accurately. Response surfaces comprising the measured moment-rotation profile and design parameters of a tape spring hinge are generated by a Box-Behnken experimental design. Furthermore, to consider deployment performances such as low latch-up load, latching without overshoot, high deployment stiffness, and high torque margin, the deployment equation is derived by Kane's dynamic equation considering any number of solar panels. The present study proposes a systematic approach for designing tape spring hinges for any number of solar panels; the designed hinges satisfy all design requirements. The approach involves minimizing the cost function including several design requirements and solving the deployment equation containing the response surfaces of the moment-rotation profiles simultaneously. To verify the effectiveness of the proposed approach, several examples are demonstrated.-
dc.languageEnglish-
dc.publisherELSEVIER FRANCE-EDITIONS SCIENTIFIQUES MEDICALES ELSEVIER-
dc.subjectPARTICLE SWARM OPTIMIZER-
dc.subjectDYNAMICS-
dc.subjectSATELLITE-
dc.titleSystematic design of tape spring hinges for solar array by optimization method considering deployment performances-
dc.typeArticle-
dc.identifier.wosid000363345500013-
dc.identifier.scopusid2-s2.0-84938066186-
dc.type.rimsART-
dc.citation.volume46-
dc.citation.beginningpage124-
dc.citation.endingpage136-
dc.citation.publicationnameAEROSPACE SCIENCE AND TECHNOLOGY-
dc.identifier.doi10.1016/j.ast.2015.06.013-
dc.contributor.localauthorPark, Youngjin-
dc.type.journalArticleArticle-
dc.subject.keywordAuthorTape spring hinge-
dc.subject.keywordAuthorSolar array deployment-
dc.subject.keywordAuthorDeployment performance-
dc.subject.keywordAuthorBox-Behnken experimental design-
dc.subject.keywordAuthorParticle swarm optimization (PSO)-
dc.subject.keywordAuthorKane&apos-
dc.subject.keywordAuthors dynamic equation-
dc.subject.keywordPlusPARTICLE SWARM OPTIMIZER-
dc.subject.keywordPlusDYNAMICS-
dc.subject.keywordPlusSATELLITE-
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