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Design and multibody dynamics analyses of the novel force-bearing structures for variable configuration spacecraft
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| Zeitschriftentitel: | Science and Engineering of Composite Materials |
|---|---|
| Personen und Körperschaften: | , , , , , |
| In: | Science and Engineering of Composite Materials, 24, 2017, 3, S. 471-476 |
| Format: | E-Article |
| Sprache: | Englisch |
| veröffentlicht: |
Walter de Gruyter GmbH
|
| Schlagwörter: |
| author_facet |
Ning, Xin Tang, Lin Gu, Junwei Liang, Chaobo Yue, Xiaokui Yuan, Jianping Ning, Xin Tang, Lin Gu, Junwei Liang, Chaobo Yue, Xiaokui Yuan, Jianping |
|---|---|
| author |
Ning, Xin Tang, Lin Gu, Junwei Liang, Chaobo Yue, Xiaokui Yuan, Jianping |
| spellingShingle |
Ning, Xin Tang, Lin Gu, Junwei Liang, Chaobo Yue, Xiaokui Yuan, Jianping Science and Engineering of Composite Materials Design and multibody dynamics analyses of the novel force-bearing structures for variable configuration spacecraft Materials Chemistry Ceramics and Composites |
| author_sort |
ning, xin |
| spelling |
Ning, Xin Tang, Lin Gu, Junwei Liang, Chaobo Yue, Xiaokui Yuan, Jianping 2191-0359 0792-1233 Walter de Gruyter GmbH Materials Chemistry Ceramics and Composites http://dx.doi.org/10.1515/secm-2015-0383 <jats:title>Abstract</jats:title> <jats:p>Novel variable configuration spacecraft (VCS) can change its configuration by on-orbit assembly or the motion of the mechanism according to the requirements and missions, and the multibody dynamics analysis is performed to obtain the corresponding theoretical lowest values of the mechanical properties of force-bearing structures for the VCS module. In the meantime, to meet the actual use requirements for VCS, novel force-bearing structures are designed optimally and fabricated successfully. The corresponding experimental values of the mechanical properties for the force-bearing structures are also tested and investigated, which are compared to the corresponding theoretical values via multibody dynamics analysis. This paper is part of a large project on the development and preparation of the novel force-bearing structures applied in the next generation of VCS.</jats:p> Design and multibody dynamics analyses of the novel force-bearing structures for variable configuration spacecraft Science and Engineering of Composite Materials |
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| title |
Design and multibody dynamics analyses of the novel force-bearing structures for variable configuration spacecraft |
| title_unstemmed |
Design and multibody dynamics analyses of the novel force-bearing structures for variable configuration spacecraft |
| title_full |
Design and multibody dynamics analyses of the novel force-bearing structures for variable configuration spacecraft |
| title_fullStr |
Design and multibody dynamics analyses of the novel force-bearing structures for variable configuration spacecraft |
| title_full_unstemmed |
Design and multibody dynamics analyses of the novel force-bearing structures for variable configuration spacecraft |
| title_short |
Design and multibody dynamics analyses of the novel force-bearing structures for variable configuration spacecraft |
| title_sort |
design and multibody dynamics analyses of the novel force-bearing structures for variable configuration spacecraft |
| topic |
Materials Chemistry Ceramics and Composites |
| url |
http://dx.doi.org/10.1515/secm-2015-0383 |
| publishDate |
2017 |
| physical |
471-476 |
| description |
<jats:title>Abstract</jats:title>
<jats:p>Novel variable configuration spacecraft (VCS) can change its configuration by on-orbit assembly or the motion of the mechanism according to the requirements and missions, and the multibody dynamics analysis is performed to obtain the corresponding theoretical lowest values of the mechanical properties of force-bearing structures for the VCS module. In the meantime, to meet the actual use requirements for VCS, novel force-bearing structures are designed optimally and fabricated successfully. The corresponding experimental values of the mechanical properties for the force-bearing structures are also tested and investigated, which are compared to the corresponding theoretical values via multibody dynamics analysis. This paper is part of a large project on the development and preparation of the novel force-bearing structures applied in the next generation of VCS.</jats:p> |
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| author | Ning, Xin, Tang, Lin, Gu, Junwei, Liang, Chaobo, Yue, Xiaokui, Yuan, Jianping |
| author_facet | Ning, Xin, Tang, Lin, Gu, Junwei, Liang, Chaobo, Yue, Xiaokui, Yuan, Jianping, Ning, Xin, Tang, Lin, Gu, Junwei, Liang, Chaobo, Yue, Xiaokui, Yuan, Jianping |
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| description | <jats:title>Abstract</jats:title> <jats:p>Novel variable configuration spacecraft (VCS) can change its configuration by on-orbit assembly or the motion of the mechanism according to the requirements and missions, and the multibody dynamics analysis is performed to obtain the corresponding theoretical lowest values of the mechanical properties of force-bearing structures for the VCS module. In the meantime, to meet the actual use requirements for VCS, novel force-bearing structures are designed optimally and fabricated successfully. The corresponding experimental values of the mechanical properties for the force-bearing structures are also tested and investigated, which are compared to the corresponding theoretical values via multibody dynamics analysis. This paper is part of a large project on the development and preparation of the novel force-bearing structures applied in the next generation of VCS.</jats:p> |
| doi_str_mv | 10.1515/secm-2015-0383 |
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| institution | DE-Gla1, DE-Zi4, DE-15, DE-Pl11, DE-Rs1, DE-105, DE-14, DE-Ch1, DE-L229, DE-D275, DE-Bn3, DE-Brt1, DE-Zwi2, DE-D161 |
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| physical | 471-476 |
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| series | Science and Engineering of Composite Materials |
| source_id | 49 |
| spelling | Ning, Xin Tang, Lin Gu, Junwei Liang, Chaobo Yue, Xiaokui Yuan, Jianping 2191-0359 0792-1233 Walter de Gruyter GmbH Materials Chemistry Ceramics and Composites http://dx.doi.org/10.1515/secm-2015-0383 <jats:title>Abstract</jats:title> <jats:p>Novel variable configuration spacecraft (VCS) can change its configuration by on-orbit assembly or the motion of the mechanism according to the requirements and missions, and the multibody dynamics analysis is performed to obtain the corresponding theoretical lowest values of the mechanical properties of force-bearing structures for the VCS module. In the meantime, to meet the actual use requirements for VCS, novel force-bearing structures are designed optimally and fabricated successfully. The corresponding experimental values of the mechanical properties for the force-bearing structures are also tested and investigated, which are compared to the corresponding theoretical values via multibody dynamics analysis. This paper is part of a large project on the development and preparation of the novel force-bearing structures applied in the next generation of VCS.</jats:p> Design and multibody dynamics analyses of the novel force-bearing structures for variable configuration spacecraft Science and Engineering of Composite Materials |
| spellingShingle | Ning, Xin, Tang, Lin, Gu, Junwei, Liang, Chaobo, Yue, Xiaokui, Yuan, Jianping, Science and Engineering of Composite Materials, Design and multibody dynamics analyses of the novel force-bearing structures for variable configuration spacecraft, Materials Chemistry, Ceramics and Composites |
| title | Design and multibody dynamics analyses of the novel force-bearing structures for variable configuration spacecraft |
| title_full | Design and multibody dynamics analyses of the novel force-bearing structures for variable configuration spacecraft |
| title_fullStr | Design and multibody dynamics analyses of the novel force-bearing structures for variable configuration spacecraft |
| title_full_unstemmed | Design and multibody dynamics analyses of the novel force-bearing structures for variable configuration spacecraft |
| title_short | Design and multibody dynamics analyses of the novel force-bearing structures for variable configuration spacecraft |
| title_sort | design and multibody dynamics analyses of the novel force-bearing structures for variable configuration spacecraft |
| title_unstemmed | Design and multibody dynamics analyses of the novel force-bearing structures for variable configuration spacecraft |
| topic | Materials Chemistry, Ceramics and Composites |
| url | http://dx.doi.org/10.1515/secm-2015-0383 |