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Deployment analysis of a planar deployable support truss structure

  • Harbin Institute of Technology
  • China Aerospace Science and Technology Corporation

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

Abstract

As the development of space structures is increasing fast, the kinematic characteristic, dynamic characteristics, driving modes and the influence of the component parameters of a planar deployable support truss structure for space antenna are discussed by means of the closed loop equations and the Kane equation. Also several examples of kinematic and dynamic analysis results under different driving modes are presented. The results show the importance of the choice of driving movements and the design of parameters and also provide a useful reference to other related truss structures.

Original languageEnglish
Title of host publication2013 IEEE International Conference on Mechatronics and Automation, IEEE ICMA 2013
Pages1287-1292
Number of pages6
DOIs
StatePublished - 2013
Event2013 10th IEEE International Conference on Mechatronics and Automation, IEEE ICMA 2013 - Takamastu, Japan
Duration: 4 Aug 20137 Aug 2013

Publication series

Name2013 IEEE International Conference on Mechatronics and Automation, IEEE ICMA 2013

Conference

Conference2013 10th IEEE International Conference on Mechatronics and Automation, IEEE ICMA 2013
Country/TerritoryJapan
CityTakamastu
Period4/08/137/08/13

Keywords

  • Kane equation
  • deployable structure
  • dynamic analysis
  • kinematic analysis

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