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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Main Authors: Fei Hu, Yanping Song, Zhirong Huang, Wenlan Liu, Wan Li
Format: Article
Language:English
Published: AIP Publishing LLC 2018-05-01
Series:AIP Advances
Online Access:http://dx.doi.org/10.1063/1.5019828
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spelling 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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