中国航空学报(英文版)2024,Vol.37Issue(3) :365-379.DOI:10.1016/j.cja.2023.07.002

Space truss construction modeling based on on-orbit assembly motion feature

Changjie ZHAO Weizhong GUO Meng CHEN Jiaxing HU Youcheng HAN Rongfu LIN
中国航空学报(英文版)2024,Vol.37Issue(3) :365-379.DOI:10.1016/j.cja.2023.07.002

Space truss construction modeling based on on-orbit assembly motion feature

Changjie ZHAO 1Weizhong GUO 1Meng CHEN 2Jiaxing HU 1Youcheng HAN 1Rongfu LIN1
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作者信息

  • 1. State Key Lab of Mechanical System and Vibration,Shanghai Jiao Tong University,Shanghai 200240,China
  • 2. Institute of Aerospace System Engineering Shanghai,Shanghai 201109,China
  • 折叠

Abstract

More space truss construction has been planned to develop and utilize space resources.These trusses are designed in the way of large-scale,complex,modular,and on-orbit assembly.To meet the upcoming challenge of large-scale space infrastructure construction,it is necessary to study space truss automation design and robotic construction.This paper proposes an ordinal finite screw adjacency matrix model(OFSAMM),focusing on the relationship between assembly motions,to express and compute a space truss structure.In this model,a space truss is abstracted as a set of ordered assembly motions,each of which is recorded as a finite screw as the basic element of the truss and its assembly.The operation of truss transformation is also derived under this model.Therefore,the truss configuration,the assembly sequence,the truss sub-assembly,the truss compo-nents,and the on-orbit assembly task can be expressed and calculated in a unified model,which is calculated and stores the truss topology and assembly with the minimum storage cost.At the end of this paper,we introduce how to synthesize and optimize space truss design through two cases.The study will help to improve design efficiency.Furthermore,it provides a theoretical basis for the automatic construction of space truss structures,especially in the next stage.

Key words

Adjacency matrix/Finite screw/On-orbit construction mod-eling/Space applications/Space trusses/Topology design

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基金项目

Manned Aerospace Research Project(040102)

出版年

2024
中国航空学报(英文版)
中国航空学会

中国航空学报(英文版)

CSTPCDEI
影响因子:0.847
ISSN:1000-9361
参考文献量36
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