DC Field | Value | Language |
---|---|---|
dc.contributor.author | Kim, Kyung Won | ko |
dc.contributor.author | Park, Youngjin | ko |
dc.date.accessioned | 2016-04-20T06:17:52Z | - |
dc.date.available | 2016-04-20T06:17:52Z | - |
dc.date.created | 2015-11-30 | - |
dc.date.created | 2015-11-30 | - |
dc.date.issued | 2015-10 | - |
dc.identifier.citation | AEROSPACE SCIENCE AND TECHNOLOGY, v.46, pp.124 - 136 | - |
dc.identifier.issn | 1270-9638 | - |
dc.identifier.uri | http://hdl.handle.net/10203/205238 | - |
dc.description.abstract | This 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.language | English | - |
dc.publisher | ELSEVIER FRANCE-EDITIONS SCIENTIFIQUES MEDICALES ELSEVIER | - |
dc.subject | PARTICLE SWARM OPTIMIZER | - |
dc.subject | DYNAMICS | - |
dc.subject | SATELLITE | - |
dc.title | Systematic design of tape spring hinges for solar array by optimization method considering deployment performances | - |
dc.type | Article | - |
dc.identifier.wosid | 000363345500013 | - |
dc.identifier.scopusid | 2-s2.0-84938066186 | - |
dc.type.rims | ART | - |
dc.citation.volume | 46 | - |
dc.citation.beginningpage | 124 | - |
dc.citation.endingpage | 136 | - |
dc.citation.publicationname | AEROSPACE SCIENCE AND TECHNOLOGY | - |
dc.identifier.doi | 10.1016/j.ast.2015.06.013 | - |
dc.contributor.localauthor | Park, Youngjin | - |
dc.type.journalArticle | Article | - |
dc.subject.keywordAuthor | Tape spring hinge | - |
dc.subject.keywordAuthor | Solar array deployment | - |
dc.subject.keywordAuthor | Deployment performance | - |
dc.subject.keywordAuthor | Box-Behnken experimental design | - |
dc.subject.keywordAuthor | Particle swarm optimization (PSO) | - |
dc.subject.keywordAuthor | Kane&apos | - |
dc.subject.keywordAuthor | s dynamic equation | - |
dc.subject.keywordPlus | PARTICLE SWARM OPTIMIZER | - |
dc.subject.keywordPlus | DYNAMICS | - |
dc.subject.keywordPlus | SATELLITE | - |
Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.