DocumentCode :
3411051
Title :
Design a High-Precision Controller of Attitude Stabilization in Wave-Measured Radar
Author :
Yuan, Gannan ; Gan, Xingli ; Zhou, Wei
Author_Institution :
Harbin Eng. Univ., Harbin
fYear :
2007
fDate :
5-8 Aug. 2007
Firstpage :
3305
Lastpage :
3309
Abstract :
With the effect of ocean wave, the motion of wave-measured radar has a periodic swing and high-frequency dither, which makes radar images have a serious polluted noise. In order to enhance the quality of radar images and realize the high stability of wave-measured radar´s attitude, the method of fuzzy-PID with repetitive control compensation (FPRCC) is designed. This method has synthesized some merits with fuzzy-PID and RCC, which has characters of high-robust and independent of mathematical model from fuzzy-PID, the characters of RCC is used to reduce the high frequency oscillation error of wave-measured radar´s attitude. From the simulation result, the conclusion is showed that the capability of fuzzy-PID with RCC is superior to fuzzy-PID, which can wipe off the sudden change of attitude movement, and realize the high-precision attitude control of wave-measured radar.
Keywords :
airborne radar; aircraft control; attitude control; fuzzy control; three-term control; attitude movement; attitude stabilization; fuzzy-PID control; high frequency oscillation error; high-frequency dither; high-precision controller; periodic swing; radar images quality; repetitive control compensation; wave-measured radar; Angular velocity control; Attitude control; Control systems; Electric motors; Radar imaging; Radar measurements; Robust control; Rotors; Tellurium; Voltage control; Attitude control; Fuzzy-PID; Repetitive control compensation; Wave-measured radar;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Mechatronics and Automation, 2007. ICMA 2007. International Conference on
Conference_Location :
Harbin
Print_ISBN :
978-1-4244-0828-3
Electronic_ISBN :
978-1-4244-0828-3
Type :
conf
DOI :
10.1109/ICMA.2007.4304092
Filename :
4304092
Link To Document :
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