Design of a New N-Shape Composite Ultra-Thin Deployable Boom in the Post-Buckling Range Using Response Surface Method and Optimization
Composite ultra-thin boom can be folded elastically. Moreover, such booms are able to self-deploy by releasing stored strain energy, which can be applied in deployable antenna, solar sail, and optical telescopes. Surrogate models for imperfection-sensitive quantities of interest and multi-objective...
| Main Authors: | , , , |
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| Format: | Article |
| Language: | English |
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IEEE
2019-01-01
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| Series: | IEEE Access |
| Subjects: | |
| Online Access: | https://ieeexplore.ieee.org/document/8794787/ |
| _version_ | 1798002003633242112 |
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| author | Hui Yang Fengshuai Lu Hongwei Guo Rongqiang Liu |
| author_facet | Hui Yang Fengshuai Lu Hongwei Guo Rongqiang Liu |
| author_sort | Hui Yang |
| collection | DOAJ |
| description | Composite ultra-thin boom can be folded elastically. Moreover, such booms are able to self-deploy by releasing stored strain energy, which can be applied in deployable antenna, solar sail, and optical telescopes. Surrogate models for imperfection-sensitive quantities of interest and multi-objective optimization are developed for the design of a new N-shape cross-section composite ultra-thin deployable boom. The proposed optimal design method integrates four general steps: (1) design of experiments, wherein the sampling designs of the N boom are created on the basis of the two-factor five-level full factorial design of experiments method; (2) efficient computational analyses of each design sample, wherein the post-buckling behavior of the N boom are analyzed under three different axial directions using nonlinear finite element ABAQUS/Explicit solver; (3) establishing the surrogate models of bending stiffness around the <inline-formula> <tex-math notation="LaTeX">$x$ </tex-math></inline-formula>-and <inline-formula> <tex-math notation="LaTeX">$y$ </tex-math></inline-formula>- axes and torsional stiffness around the <inline-formula> <tex-math notation="LaTeX">$z$ </tex-math></inline-formula>-axis by response surface method (RSM); (4) performing the multi-objective optimization design using modified non-dominated sorting genetic algorithm to realize the optimal design. The bending stiffness around the <inline-formula> <tex-math notation="LaTeX">$x$ </tex-math></inline-formula>-and <inline-formula> <tex-math notation="LaTeX">$y$ </tex-math></inline-formula>- axes and the torsional stiffness around the <inline-formula> <tex-math notation="LaTeX">$z$ </tex-math></inline-formula>-axis are set as the objectives, mass is set as the constraint, and the bonded web height and the central angle of the middle tape spring of the N boom are set as the variables. The typical surrogate modeling method can be applied to different problems in structural and material design. |
| first_indexed | 2024-04-11T11:45:16Z |
| format | Article |
| id | doaj.art-3e717211f6c548a8bbbd394cdfc56933 |
| institution | Directory Open Access Journal |
| issn | 2169-3536 |
| language | English |
| last_indexed | 2024-04-11T11:45:16Z |
| publishDate | 2019-01-01 |
| publisher | IEEE |
| record_format | Article |
| series | IEEE Access |
| spelling | doaj.art-3e717211f6c548a8bbbd394cdfc569332022-12-22T04:25:35ZengIEEEIEEE Access2169-35362019-01-01712965912966510.1109/ACCESS.2019.29347448794787Design of a New N-Shape Composite Ultra-Thin Deployable Boom in the Post-Buckling Range Using Response Surface Method and OptimizationHui Yang0Fengshuai Lu1Hongwei Guo2https://orcid.org/0000-0001-7498-6755Rongqiang Liu3College of Electrical Engineering and Automation, Anhui University, Hefei, ChinaCollege of Electrical Engineering and Automation, Anhui University, Hefei, ChinaChina State Key Laboratory of Robotics and System, Harbin Institute of Technology, Harbin, ChinaChina State Key Laboratory of Robotics and System, Harbin Institute of Technology, Harbin, ChinaComposite ultra-thin boom can be folded elastically. Moreover, such booms are able to self-deploy by releasing stored strain energy, which can be applied in deployable antenna, solar sail, and optical telescopes. Surrogate models for imperfection-sensitive quantities of interest and multi-objective optimization are developed for the design of a new N-shape cross-section composite ultra-thin deployable boom. The proposed optimal design method integrates four general steps: (1) design of experiments, wherein the sampling designs of the N boom are created on the basis of the two-factor five-level full factorial design of experiments method; (2) efficient computational analyses of each design sample, wherein the post-buckling behavior of the N boom are analyzed under three different axial directions using nonlinear finite element ABAQUS/Explicit solver; (3) establishing the surrogate models of bending stiffness around the <inline-formula> <tex-math notation="LaTeX">$x$ </tex-math></inline-formula>-and <inline-formula> <tex-math notation="LaTeX">$y$ </tex-math></inline-formula>- axes and torsional stiffness around the <inline-formula> <tex-math notation="LaTeX">$z$ </tex-math></inline-formula>-axis by response surface method (RSM); (4) performing the multi-objective optimization design using modified non-dominated sorting genetic algorithm to realize the optimal design. The bending stiffness around the <inline-formula> <tex-math notation="LaTeX">$x$ </tex-math></inline-formula>-and <inline-formula> <tex-math notation="LaTeX">$y$ </tex-math></inline-formula>- axes and the torsional stiffness around the <inline-formula> <tex-math notation="LaTeX">$z$ </tex-math></inline-formula>-axis are set as the objectives, mass is set as the constraint, and the bonded web height and the central angle of the middle tape spring of the N boom are set as the variables. The typical surrogate modeling method can be applied to different problems in structural and material design.https://ieeexplore.ieee.org/document/8794787/Deployable structuresN boombucklingresponse surface methodoptimization |
| spellingShingle | Hui Yang Fengshuai Lu Hongwei Guo Rongqiang Liu Design of a New N-Shape Composite Ultra-Thin Deployable Boom in the Post-Buckling Range Using Response Surface Method and Optimization IEEE Access Deployable structures N boom buckling response surface method optimization |
| title | Design of a New N-Shape Composite Ultra-Thin Deployable Boom in the Post-Buckling Range Using Response Surface Method and Optimization |
| title_full | Design of a New N-Shape Composite Ultra-Thin Deployable Boom in the Post-Buckling Range Using Response Surface Method and Optimization |
| title_fullStr | Design of a New N-Shape Composite Ultra-Thin Deployable Boom in the Post-Buckling Range Using Response Surface Method and Optimization |
| title_full_unstemmed | Design of a New N-Shape Composite Ultra-Thin Deployable Boom in the Post-Buckling Range Using Response Surface Method and Optimization |
| title_short | Design of a New N-Shape Composite Ultra-Thin Deployable Boom in the Post-Buckling Range Using Response Surface Method and Optimization |
| title_sort | design of a new n shape composite ultra thin deployable boom in the post buckling range using response surface method and optimization |
| topic | Deployable structures N boom buckling response surface method optimization |
| url | https://ieeexplore.ieee.org/document/8794787/ |
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