DocumentCode :
1868274
Title :
Static analysis of synchronism deployable antenna
Author :
Guan, Fuling ; Shou, Jianjun ; Zhang, Jingjie
Author_Institution :
Dept. of Civil Eng., Zhejiang Univ., Hangzhou
fYear :
2006
fDate :
19-21 Jan. 2006
Lastpage :
1424
Abstract :
A 3-dimensions synchronism deployable antenna had been designed, analyzed, and manufactured by our research group. This antenna consists of tetrahedral elements from central element. Because there are springs at the ends of some of the rods, spider joints are applied. For analysis purpose, the structure is simplified and modeled by using two dimensional beam elements that have no bending stiffness. Displacement vectors are defined to include two translational displacements and one torsional displacement. The stiffness matrix derived by this method is relatively simple and well defined. The analysis results generated by using software developed by our research group, agreed very well with available test data
Keywords :
antenna theory; beam steering; matrix algebra; space vehicle antennas; synchronisation; torsion; 2D beam elements; 3D deployable antenna; displacement vectors; spider joints; static analysis; stiffness matrix; synchronism deployable antenna; tetrahedral elements; torsional displacement; translational displacements; Capacitive sensors; Equations; Gravity; Loaded antennas; Manufacturing; Matrices; Performance analysis; Springs; Stress; Structural rods;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Systems and Control in Aerospace and Astronautics, 2006. ISSCAA 2006. 1st International Symposium on
Conference_Location :
Harbin
Print_ISBN :
0-7803-9395-3
Type :
conf
DOI :
10.1109/ISSCAA.2006.1627504
Filename :
1627504
Link To Document :
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