Deployment analysis of a planar deployable support truss structure

Author

Dandan Wang ; Rongqiang Liu ; Yan Wang ; Hongwei Guo ; Qiang Cong ; Congfa Zhang

Author_Institution

Sch. of Mech. & Electr. Eng., Harbin Inst. of Technol., Harbin, China

fYear

2013

fDate

4-7 Aug. 2013

Firstpage

1287

Lastpage

1292

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.

Keywords

aerospace engineering; design engineering; structural engineering; supports; Kane equation; closed loop equations; design; driving movements; dynamic analysis; kinematic analysis; planar deployable support truss structure; space antenna; space structure development; Angular velocity; Equations; Force; Kinematics; Mathematical model; Space vehicles; Torque; Kane equation; deployable structure; dynamic analysis; kinematic analysis;

fLanguage

English

Publisher

ieee

Conference_Titel

Mechatronics and Automation (ICMA), 2013 IEEE International Conference on

Conference_Location

Takamatsu

Print_ISBN

978-1-4673-5557-5

Type

conf

DOI

10.1109/ICMA.2013.6618099

Filename

6618099