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
Link To Document :
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