Malleability and optimization of tetrahedral metamorphic element for deployable truss antenna reflector
The tetrahedral elements that make up the large deployable reflector (LDR) are a kind of metamorphic element, which belongs to the multi-loop coupling mechanism. Firstly, the method of combining topology with screw theory is put forward. The parametric model and the constrained matrix are establishe...
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doaj-739be6b032464286bc5219b847a264e32020-11-24T22:09:46ZengAIP Publishing LLCAIP Advances2158-32262018-05-0185055217055217-1010.1063/1.5019828011805ADVMalleability and optimization of tetrahedral metamorphic element for deployable truss antenna reflectorFei Hu0Yanping Song1Zhirong Huang2Wenlan Liu3Wan Li4China Academy of Space Technology (Xi’an), Xi’an 710100, ChinaChina Academy of Space Technology (Xi’an), Xi’an 710100, ChinaChina Academy of Space Technology (Xi’an), Xi’an 710100, ChinaParallel Robot and Mechatronic System Laboratory of Hebei Province, Yanshan University, Qinhuangdao 066004, ChinaSchool of Computer Science and Technology, Xidian University, Xi’an 710100, ChinaThe tetrahedral elements that make up the large deployable reflector (LDR) are a kind of metamorphic element, which belongs to the multi-loop coupling mechanism. Firstly, the method of combining topology with screw theory is put forward. The parametric model and the constrained matrix are established to analyze the malleability of 3RR-3RRR tetrahedral element. Secondly, the kinematics expression of each motion pair is deduced by the relationship between the velocity and the motion spinor. Finally, the configuration of the metamorphic element is optimized to make the parabolic antenna fully folded, so that the antenna can meet the maximum folding ratio. The results show that the 3RR-3RRR element is a single-degree of freedom (DOF) mechanism. What’s more, three new configurations 3RS-3RRR, 3SR-3RRR and 3UU-3RRR are obtained on the basis of optimization. In particular, it proves to be that the LDR which consists of the 3RS-3RRR metamorphic element can achieve the maximum folding ratio. This paper provides a theoretical basis for the computer-aided design of the truss antennas, which has an excellent applicability in the field of aerospace and other multi-loop coupling mechanism.http://dx.doi.org/10.1063/1.5019828 |
collection |
DOAJ |
language |
English |
format |
Article |
sources |
DOAJ |
author |
Fei Hu Yanping Song Zhirong Huang Wenlan Liu Wan Li |
spellingShingle |
Fei Hu Yanping Song Zhirong Huang Wenlan Liu Wan Li Malleability and optimization of tetrahedral metamorphic element for deployable truss antenna reflector AIP Advances |
author_facet |
Fei Hu Yanping Song Zhirong Huang Wenlan Liu Wan Li |
author_sort |
Fei Hu |
title |
Malleability and optimization of tetrahedral metamorphic element for deployable truss antenna reflector |
title_short |
Malleability and optimization of tetrahedral metamorphic element for deployable truss antenna reflector |
title_full |
Malleability and optimization of tetrahedral metamorphic element for deployable truss antenna reflector |
title_fullStr |
Malleability and optimization of tetrahedral metamorphic element for deployable truss antenna reflector |
title_full_unstemmed |
Malleability and optimization of tetrahedral metamorphic element for deployable truss antenna reflector |
title_sort |
malleability and optimization of tetrahedral metamorphic element for deployable truss antenna reflector |
publisher |
AIP Publishing LLC |
series |
AIP Advances |
issn |
2158-3226 |
publishDate |
2018-05-01 |
description |
The tetrahedral elements that make up the large deployable reflector (LDR) are a kind of metamorphic element, which belongs to the multi-loop coupling mechanism. Firstly, the method of combining topology with screw theory is put forward. The parametric model and the constrained matrix are established to analyze the malleability of 3RR-3RRR tetrahedral element. Secondly, the kinematics expression of each motion pair is deduced by the relationship between the velocity and the motion spinor. Finally, the configuration of the metamorphic element is optimized to make the parabolic antenna fully folded, so that the antenna can meet the maximum folding ratio. The results show that the 3RR-3RRR element is a single-degree of freedom (DOF) mechanism. What’s more, three new configurations 3RS-3RRR, 3SR-3RRR and 3UU-3RRR are obtained on the basis of optimization. In particular, it proves to be that the LDR which consists of the 3RS-3RRR metamorphic element can achieve the maximum folding ratio. This paper provides a theoretical basis for the computer-aided design of the truss antennas, which has an excellent applicability in the field of aerospace and other multi-loop coupling mechanism. |
url |
http://dx.doi.org/10.1063/1.5019828 |
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