DocumentCode :
518017
Title :
Lift control system improved on single wing fin stabilizer at zero speed
Author :
Chunmei, Hua ; Yu, Wang ; Shuyan, Ding ; Man, Li ; Weiguang, Zhao
Author_Institution :
Sch. of Electr. & Commun. Eng., Heilongjiang Inst. of Sci. & Technol., Harbin, China
Volume :
4
fYear :
2010
fDate :
16-18 April 2010
Abstract :
It is different from conventional ship fin stabilizer that the lift of fin stabilizer is produced by initiative swing of movement mode of pitching and heaving at zero speed. For the fin stabilizer is belong to bigger inertia load, the reverse lift could be generated with the shorter braking time and the ship rolling would be acute and getting worse. So the lift limit element should be improved and lift limit is introduced. 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. And the anti rolling effects achieved over 55% 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 :
braking; controllers; ships; anti rolling effect; braking time; inertia load; lift control system; lift limit element; reverse lift; sea wave; ship fin stabilizer; ship rolling; single wing fin stabilizer; zero forward speed; Communication system control; Control engineering education; Control systems; Educational technology; Feedback; Marine vehicles; Navigation; Sea surface; Servomechanisms; Velocity control; anti rolling ship; control system; fin stabilizers; lift feedback; zero forward speed;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Computer Engineering and Technology (ICCET), 2010 2nd International Conference on
Conference_Location :
Chengdu
Print_ISBN :
978-1-4244-6347-3
Type :
conf
DOI :
10.1109/ICCET.2010.5485449
Filename :
5485449
Link To Document :
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