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contributor authorCao, Wen-ao
contributor authorXi, Sheng
contributor authorDing, Huafeng
contributor authorChen, Ziming
date accessioned2022-02-06T05:45:53Z
date available2022-02-06T05:45:53Z
date copyright7/19/2021 12:00:00 AM
date issued2021
identifier issn1050-0472
identifier othermd_143_12_124502.pdf
identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4278707
description abstractThis paper aims to present the topological structure design and kinematic analysis of a novel double-ring truss deployable satellite antenna mechanism. First, a new topological scheme and a new rectangular prism deployable linkage unit are proposed for constructing the kind of antenna mechanisms. Second, the degree-of-freedom (DOF) of the deployable unit and the antenna mechanism are analyzed based on structure decomposition and screw theory. Third, the kinematic model of the double-ring truss deployable antenna mechanism is established based on its structural characteristics. Finally, a typical numerical example is used to illustrate the effectiveness of the designed mechanism and the established kinematic model. The new double-ring truss deployable antenna mechanism consists of the units with the better structural symmetry and has simpler joint axis layouts, comparing with the same type of most existing mechanisms.
publisherThe American Society of Mechanical Engineers (ASME)
titleDesign and Kinematics of a Novel Double-Ring Truss Deployable Antenna Mechanism
typeJournal Paper
journal volume143
journal issue12
journal titleJournal of Mechanical Design
identifier doi10.1115/1.4051352
journal fristpage0124502-1
journal lastpage0124502-9
page9
treeJournal of Mechanical Design:;2021:;volume( 143 ):;issue: 012
contenttypeFulltext


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