Volume 39 Issue 2
Mar.  2019
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LUO Ani, LIU Heping. Analysis for the Star-tensegrity Deployable Structure[J]. Journal of Space Science, 2019, 39(2): 222-227. doi: 10.11728/cjss2019.02.222
Citation: LUO Ani, LIU Heping. Analysis for the Star-tensegrity Deployable Structure[J]. Journal of Space Science, 2019, 39(2): 222-227. doi: 10.11728/cjss2019.02.222

Analysis for the Star-tensegrity Deployable Structure

doi: 10.11728/cjss2019.02.222
  • Received Date: 2018-05-23
  • Rev Recd Date: 2018-10-15
  • Publish Date: 2019-03-15
  • A star-tensegrity deployable structure is presented. It is formed through transforming the star tensegrity structure and can be driven by a central member to complete folding and deploying. Firstly, based on the tensegrity unit, the star-tensegrity structure is presented and the scheme for the star-tensegrity deployable structure is investigated. Then how to drive it is discussed and determined. Finally, the influence of the central member length on the structural and force parameters is analyzed. Through theoretical analysis and simulation, the feasibility for folding and deploying of the star-tensegrity deployable structure is checked and verified. The results show that a feasible star-tensegrity deployable structure is obtained.

     

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