Multibody Analysis of the Force in Deploying Booms-Reference-Cited by-同舟云学术

Multibody Analysis of the Force in Deploying Booms

Published:2013-11 Issue:6 Volume:36 Page:1881-1886
ISSN:0731-5090
Container-title:Journal of Guidance, Control, and Dynamics
language:en
Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Wu Jiang¹,Zhao Zhihua¹,Ren Gexue¹

Affiliation:

1. Department of Engineering Physics, Tsinghua University, 100084 Beijing, People’s Republic of China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.60296

Reference15 articles.

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2. Large retractable appendages in spacecraft

3. TibertG. “Deployable Tensegrity Structures for Space Applications,” Ph.D. Thesis, Dept. of Mechanics, Royal Institute of Technology, Stockholm, 2002.

4. GlaserD. L. “Mechanical System Design of the CubeSat for Ions, Electrons, Neutrals, and Magnetic Fields Mission (CINEMA),” M.S. Thesis, Mechanical Engineering Dept. Univ. of California, Berkeley, CA, 2009.

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