DocumentCode
1868772
Title
Error model and vibration analysis of Timoshenko beam subjected to a moving mass
Author
Qu, Zhiyong ; Yao, Yu
Author_Institution
Harbin Inst. of Technol.
fYear
2006
fDate
19-21 Jan. 2006
Lastpage
1281
Abstract
The 6-DOF simulation system has many error factors. To reduce error magnitude and raise simulation precision, the error model is established. By analyzing the basic rules of system with error, the composing method of characteristic matrix can be put forward. Based on characteristic matrix and multi-body kinematics, synthesis error model including static and dynamic errors are obtained. The dynamic response and vibration of beam, which is subjected to a moving table, is chiefly analyzed. Based on Timoshenko´s beam theory and Euler-Lagrange equation, the equations of motion for the beam system, which are composed of translation errors and rotation errors of beam, are obtained. This method can offer academic reference to error synthesis model and compensation for 6-DOF simulation system
Keywords
beams (structures); error analysis; kinematics; motion control; vibrations; 6-DOF simulation system; Euler-Lagrange equation; Timoshenko beam; beam system; beam theory; characteristic matrix; error factors; error synthesis model; motion equations; multibody kinematics; rotation errors; translation errors; vibration analysis; Analytical models; Computational modeling; Computer errors; Computer simulation; Equations; Error analysis; Kinematics; Manufacturing; Missiles; Motion analysis;
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.2006.1627520
Filename
1627520
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