KINEMATIC ANALYSIS OF THE DEPLOYABLE TRUSS STRUCTURES FOR SPACE APPLICATIONS doi: 10.5028/jatm.2012.04044112
Deployable structure technology has been used in aerospace and civil engineering structures very popularly. This paper reported on a recent development of numerical approaches for the kinematic analysis of the deployable truss structures. The dynamic equations of the constrained system and the compu...
Main Authors: | , , , |
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Format: | Article |
Language: | English |
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Instituto de Aeronáutica e Espaço (IAE)
2012-12-01
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Series: | Journal of Aerospace Technology and Management |
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Online Access: | https://www.jatm.com.br/jatm/article/view/215 |
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author | Xu Yan Guan Fu-ling Zheng Yao Zhao Mengliang |
author_facet | Xu Yan Guan Fu-ling Zheng Yao Zhao Mengliang |
author_sort | Xu Yan |
collection | DOAJ |
description | Deployable structure technology has been used in aerospace and civil engineering structures very popularly. This paper reported on a recent development of numerical approaches for the kinematic analysis of the deployable truss structures. The dynamic equations of the constrained system and the computational procedures were summarized. The driving force vectors of the active cables considering the friction force were also formulated. Three types of macroelements used in deployable structures were described, including linear scissor-link element, multiangular scissor element, and rigid-plate element. The corresponding constraint equations and the Jacobian matrices of these macroelements were formulated. The accuracy and efficiency of the proposed approach are illustrated with numerical examples, including a double-ring deployable truss and a deployable solar array. |
first_indexed | 2024-04-14T03:48:24Z |
format | Article |
id | doaj.art-f5b4b5ce35cf42c6b7346baf61cb847e |
institution | Directory Open Access Journal |
issn | 2175-9146 |
language | English |
last_indexed | 2024-04-14T03:48:24Z |
publishDate | 2012-12-01 |
publisher | Instituto de Aeronáutica e Espaço (IAE) |
record_format | Article |
series | Journal of Aerospace Technology and Management |
spelling | doaj.art-f5b4b5ce35cf42c6b7346baf61cb847e2022-12-22T02:14:09ZengInstituto de Aeronáutica e Espaço (IAE)Journal of Aerospace Technology and Management2175-91462012-12-0144KINEMATIC ANALYSIS OF THE DEPLOYABLE TRUSS STRUCTURES FOR SPACE APPLICATIONS doi: 10.5028/jatm.2012.04044112Xu Yan0Guan Fu-ling1Zheng Yao2Zhao Mengliang3Zhejiang University HangzhouZhejiang University HangzhouZhejiang University HangzhouZhejiang University Hangzhou Shanghai JiangNan Architectural Design InstituteDeployable structure technology has been used in aerospace and civil engineering structures very popularly. This paper reported on a recent development of numerical approaches for the kinematic analysis of the deployable truss structures. The dynamic equations of the constrained system and the computational procedures were summarized. The driving force vectors of the active cables considering the friction force were also formulated. Three types of macroelements used in deployable structures were described, including linear scissor-link element, multiangular scissor element, and rigid-plate element. The corresponding constraint equations and the Jacobian matrices of these macroelements were formulated. The accuracy and efficiency of the proposed approach are illustrated with numerical examples, including a double-ring deployable truss and a deployable solar array.https://www.jatm.com.br/jatm/article/view/215Kinematic analysisDeployable truss structuresMacroelementsDeployable solar array. |
spellingShingle | Xu Yan Guan Fu-ling Zheng Yao Zhao Mengliang KINEMATIC ANALYSIS OF THE DEPLOYABLE TRUSS STRUCTURES FOR SPACE APPLICATIONS doi: 10.5028/jatm.2012.04044112 Journal of Aerospace Technology and Management Kinematic analysis Deployable truss structures Macroelements Deployable solar array. |
title | KINEMATIC ANALYSIS OF THE DEPLOYABLE TRUSS STRUCTURES FOR SPACE APPLICATIONS doi: 10.5028/jatm.2012.04044112 |
title_full | KINEMATIC ANALYSIS OF THE DEPLOYABLE TRUSS STRUCTURES FOR SPACE APPLICATIONS doi: 10.5028/jatm.2012.04044112 |
title_fullStr | KINEMATIC ANALYSIS OF THE DEPLOYABLE TRUSS STRUCTURES FOR SPACE APPLICATIONS doi: 10.5028/jatm.2012.04044112 |
title_full_unstemmed | KINEMATIC ANALYSIS OF THE DEPLOYABLE TRUSS STRUCTURES FOR SPACE APPLICATIONS doi: 10.5028/jatm.2012.04044112 |
title_short | KINEMATIC ANALYSIS OF THE DEPLOYABLE TRUSS STRUCTURES FOR SPACE APPLICATIONS doi: 10.5028/jatm.2012.04044112 |
title_sort | kinematic analysis of the deployable truss structures for space applications doi 10 5028 jatm 2012 04044112 |
topic | Kinematic analysis Deployable truss structures Macroelements Deployable solar array. |
url | https://www.jatm.com.br/jatm/article/view/215 |
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