• 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