DocumentCode
2850676
Title
Distributed rudder control system based on CAN bus
Author
Wu, Zhigang ; Liu, Qinglin ; Peng, Xianmin ; Chen, Zurong ; Tang, Qiaoqiao
Author_Institution
China Aerodynamics R&D Center, Mianyang, China
fYear
2012
fDate
24-27 June 2012
Firstpage
210
Lastpage
212
Abstract
In order to change rudder angle of the models in the wind tunnel test, a rudder control system (RCS) based on CAN bus was designed. Through the rudder angle regulating by the feedback of Linearity variable differential transducer (LVDT), the RCS achieves high precision control. We present the makeup, principle, and design of hardware and software of RCS. According to the wind tunnel test, the RCS works well, the control precision achieves the design target as expect and the test data meet the needs.
Keywords
control system synthesis; controller area networks; distributed control; feedback; field buses; spatial variables control; transducers; wind tunnels; CAN bus; LVDT feedback; RCS design; RCS hardware design; RCS software design; distributed rudder control system; high precision control; linearity variable differential transducer feedback; rudder angle regulation; wind tunnel test; Irrigation; CAN bus; LVDT; rudder control; wind tunnel test;
fLanguage
English
Publisher
ieee
Conference_Titel
Electrical & Electronics Engineering (EEESYM), 2012 IEEE Symposium on
Conference_Location
Kuala Lumpur
Print_ISBN
978-1-4673-2363-5
Type
conf
DOI
10.1109/EEESym.2012.6258626
Filename
6258626
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