DocumentCode :
2709340
Title :
Research on Lift Control System of Single Wing Fin Stabilizer at Zero Speed
Author :
Chunmei, Hua ; Yu, Wang ; Man, Li ; Shuyan, Ding ; Zongyan, Yu
Author_Institution :
Sch. of Electr. & Commun. Eng., Heilongjiang Inst. of Sci. & Technol., Harbin, China
fYear :
2010
fDate :
7-10 May 2010
Firstpage :
811
Lastpage :
814
Abstract :
The technique is a kind of new concept of anti rolling ship at zero forward speed. It is different from conventional ship fin stabilizer that the lift of fin stabilizer based on movement mode of pitching and heaving is produced by initiative swing at zero speed. The lift control system is built according to lift feedback and lift limit. It is undoubtedly another development to introduce lift control to ship roll stabilization at zero forward speed. The simulation of anti rolling effect is researched at the different sea wave condition about significant wave height is 1 m and 2 m, wave direction angle is 90 . And the anti rolling effects are 78.30% and 56.92%respectively. It is proved that the designed system could be satisfied with the need of anti rolling ship at zero speed. This research is supported by the science and technology research project of Education Department of Heilongjiang Province (11544044).
Keywords :
control systems; controllers; motion control; ships; velocity control; Education Department of Heilongjiang Province; lift control system; ship roll stabilization; single wing fin stabilizer; zero forward speed; Communication system control; Control systems; Educational technology; Feedback; Frequency; Marine vehicles; Navigation; Research and development; Servomechanisms; Velocity control; anti rolling ship; control system; fin stabilizers; lift feedback; zero forward speed;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Computer Research and Development, 2010 Second International Conference on
Conference_Location :
Kuala Lumpur
Print_ISBN :
978-0-7695-4043-6
Type :
conf
DOI :
10.1109/ICCRD.2010.148
Filename :
5489482
Link To Document :
بازگشت