Please use this identifier to cite or link to this item: http://hdl.handle.net/10397/110007
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dc.contributorDepartment of Mechanical Engineering-
dc.creatorTan, G-
dc.creatorMeng, X-
dc.creatorDuan, X-
dc.creatorCheng, L-
dc.creatorNiu, D-
dc.creatorHe, S-
dc.creatorZhang, D-
dc.date.accessioned2024-11-20T07:30:49Z-
dc.date.available2024-11-20T07:30:49Z-
dc.identifier.issn2096-3459-
dc.identifier.urihttp://hdl.handle.net/10397/110007-
dc.language.isoenen_US
dc.publisherKeAi Publishing Communications Ltd.en_US
dc.rights© 2024 China Ordnance Society. Publishing services by Elsevier B.V. on behalf of KeAi Communications Co. Ltd. This is an open access article under the CC BY license (http://creativecommons.org/licenses/by/4.0/).en_US
dc.rightsThe following publication Tan, G., Meng, X., Duan, X., Cheng, L., Niu, D., He, S., & Zhang, D. (2024). Kinematic-mapping-model-guided analysis and optimization of 2-PSS&1-RR circular-rail parallel mechanism for fully steerable phased array antennas. Defence Technology, 38, 136-154 is available at https://doi.org/10.1016/j.dt.2024.03.001.en_US
dc.subjectBacktrackingen_US
dc.subjectCircular railen_US
dc.subjectCrank-slider linkageen_US
dc.subjectInnovative antenna mounten_US
dc.subjectKinematic mapping modelen_US
dc.subjectStiffness singularityen_US
dc.titleKinematic-mapping-model-guided analysis and optimization of 2-PSS&1-RR circular-rail parallel mechanism for fully steerable phased array antennasen_US
dc.typeJournal/Magazine Articleen_US
dc.identifier.spage136-
dc.identifier.epage154-
dc.identifier.volume38-
dc.identifier.doi10.1016/j.dt.2024.03.001-
dcterms.abstractThis paper presents a systematic methodology for analyzing and optimizing an innovative antenna mount designed for phased array antennas, implemented through a novel 2-PSS&1-RR circular-rail parallel mechanism. Initially, a comparative motion analysis between the 3D model of the mount and its full-scale prototype is conducted to validate effectiveness. Given the inherent complexity, a kinematic mapping model is established between the mount and the crank-slider linkage, providing a guiding framework for subsequent analysis and optimization. Guided by this model, feasible inverse and forward solutions are derived, enabling precise identification of stiffness singularities. The concept of singularity distance is thus introduced to reflect the structural stiffness of the mount. Subsequently, also guided by the mapping model, a heuristic algorithm incorporating two backtracking procedures is developed to reduce the mount's mass. Additionally, a parametric finite-element model is employed to explore the relation between singularity distance and structural stiffness. The results indicate a significant reduction (about 16%) in the antenna mount's mass through the developed algorithm, while highlighting the singularity distance as an effective stiffness indicator for this type of antenna mount.-
dcterms.abstractGraphical abstract: [Figure not available: see fulltext.]-
dcterms.accessRightsopen accessen_US
dcterms.bibliographicCitationDefence technology, Aug. 2024, v. 38, p. 136-154-
dcterms.isPartOfDefence technology-
dcterms.issued2024-08-
dc.identifier.scopus2-s2.0-85189690729-
dc.identifier.eissn2214-9147-
dc.description.validate202411 bcch-
dc.description.oaVersion of Recorden_US
dc.identifier.FolderNumberOA_Scopus/WOSen_US
dc.description.fundingSourceOthersen_US
dc.description.fundingTextNational Key Research and Development Program of China, High efficiency space satellite charging system based on microwave wireless energy transfer technologyen_US
dc.description.pubStatusPublisheden_US
dc.description.oaCategoryCCen_US
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