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Dynamics of Space Deployable Structures

[+] Author Affiliations
Qiang Tian, Cheng Liu, Chunyan Zhou, Haiyan Hu

Beijing Institute of Technology, Beijing, China

Jiang Zhao

Xi’an Institute of Space Radio Technology, Xi’an, Shaanxi, China

Paper No. DETC2015-46159, pp. V006T10A010; 8 pages
doi:10.1115/DETC2015-46159
From:
  • ASME 2015 International Design Engineering Technical Conferences and Computers and Information in Engineering Conference
  • Volume 6: 11th International Conference on Multibody Systems, Nonlinear Dynamics, and Control
  • Boston, Massachusetts, USA, August 2–5, 2015
  • Conference Sponsors: Design Engineering Division, Computers and Information in Engineering Division
  • ISBN: 978-0-7918-5716-8
  • Copyright © 2015 by ASME

abstract

The space industry is eager to have the advanced technology of large space structures composed of trusses, cables and meshes. These space structures will deploy on orbit for different space missions. The important scientific basis of the technology is the nonlinear dynamic modeling, analysis and control of those space structures during their deployment and service. In this study, many space deployable structures (such as satellites antenna and spinning solar sail) are described by using the absolute nodal coordinate formulation (ANCF), and the huge set of equations of motion are solve by high efficient parallel generalized-alpha method. Some numerical results are also validated by experiment results.

Copyright © 2015 by ASME

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