Equivalent Dynamic Model of the Space Antenna Truss with Initial Stress-Reference-Cited by-同舟云学术

Equivalent Dynamic Model of the Space Antenna Truss with Initial Stress

Published:2020-04 Issue:4 Volume:58 Page:1851-1863
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Liu Mei¹,Cao Dengqing¹,Zhu Dongfang²

Affiliation:

1. Harbin Institute of Technology, 150001 Harbin, People’s Republic of China

2. Shanghai Aerospace Control Technology Institute, 201109 Shanghai, People’s Republic of China

Funder

Civil Aerospace Project

National Natural Science Foundation of China

Natural Science Foundation of Shanghai City, PR China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference30 articles.

1. A review on large deployable structures for astrophysics missions

2. TibertG. “Deployable Tensegrity Structures for Space Applications,” Ph.D. Dissertation, Dept. of Mechanics, Royal Inst. of Technology, Stockholm, Sweden, 2002, pp. 1–2.

3. Design of tensegrity structures for supporting deployable mesh antennas

4. Concept of the tension truss antenna

5. Semi-Active Friction Damping of Large Space Truss Structures

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