期刊文献+

基于LMI的船舶主鳍/襟翼鳍鲁棒控制研究 被引量:1

Research on Robust Control of Ship Main/Flap Fin Stabilizer Based on LMI
下载PDF
导出
摘要 针对随机海浪干扰、未建模动态和模型参数不确定性,建立船舶主鳍/襟翼鳍系统数学模型,基于线性矩阵不等式(LMI)的H∞控制方法,考虑干扰抑制、控制器输出约束和模型不确定性的混合灵敏度问题,应用回路成形方法,设计了H∞控制器,详细地分析设计中的权函数选择和灵敏度函数特性等问题,通过仿真验证了这一方法的可行性,所设计的船舶主鳍/襟翼鳍减摇系统不但可以有效地减小船舶横摇,而且系统具有很好的鲁棒稳定性,同时,满足主鳍/襟翼鳍的鳍角幅值约束条件。 For ship disturbed by sea wave, neglected dynamics and parametric uncertainties, the math model of main/flap fin stabilizer system was set up. Considering reducing disturbance, control constraints and model uncertainties, H ∞ robust controller of ship fin stabilizer system was designed which introduced Linear Matrix Inequality solution to achieve the desired improvement in system performance by applying loop shaping methods. Furthermore, performance weighting functions, characteristic of sensitivity functions, etc. were investigated. The method is proved to be feasible because the ship main/flap fin stabilizer system can not only reduce ship roll but also possess robust stability, and angle constraints of main/ flap fin are satisfied.
出处 《系统仿真学报》 EI CAS CSCD 北大核心 2008年第12期3250-3252,3257,共4页 Journal of System Simulation
关键词 海浪干扰 主鳍/襟翼鳍 H∞控制 LMI 混合灵敏度S/R/T问题 sea wave disturbance main/flap fin stabilizer H∞ control LMI mixed sensitivity problem S / R/T
  • 相关文献

参考文献6

  • 1Gahinet P, Apkarian P. An LMI-based parameterization of all H∞ controllers with applications [C]//IEEE 32th Conference on Decision and Control (S0191-2216). USA: IEEE, 1993: 656-661.
  • 2Gahinet P, Apkarian P. A linear matrix inequality approach to H∞ control [J]. International Journal of Robust and Nonlinear Control (S1049-8923), 1994, 4(1): 421-448.
  • 3Iwasaki T, Skelton R E. All controllers for the general H∞ control problem: LMI existence conditions and state space formulas [J]. Automatica (S0005-1098), 1994, 30(8): 1307-1317.
  • 4Gahinet E Explicit controller formulas for LMI-based H∞ synthesis [J]. Automatica (S0005-1098), 1996, 32(7): 1007-1014.
  • 5Fujimori A. Optimization of static output feedback using substitutive LMI formulation [J]. IEEE Transactions on Automatic Control (S0018-9286), 2004, 6(49): 995-999.
  • 6李友年,贾晓洪,王海波,刘忠.反作用射流控制导弹的自动驾驶仪H_∞设计方法[J].系统仿真学报,2005,17(7):1771-1773. 被引量:2

二级参考文献5

  • 1康志敏.高超声速飞行器发展战略研究[J].现代防御技术,2000,28(4):27-33. 被引量:9
  • 2陈佳实.导弹制导和控制系统的分析与设计[M].北京:宇航出版社,1989..
  • 3Rui Hirokawa, Koichi Sato. Autopilot Design for a Missile with Reaction-jet Using Coefficient Diagram Method [A]. AIAA GUIDANCE, NAVIGATION, AND CONTROL CONFERENCE [C].2001, 739-746.
  • 4Roark D.Weil, Kevin A.Wise. Blended Aero & Reaction Jet Missile Autopilot Design Using VSS Techniques [A]. Proceedings of the 30th Conference on Decision and Control [C]. 2828-2829.
  • 5Ajay Thukral, Mario Innocenti. A Sliding Mode Missile Pitch Autopilot Synethesis for High Angle of Attack Maneuvering [J].IEEE Transactions on Control Systems Technology, 1998, 6(3):359-371.

共引文献1

同被引文献7

引证文献1

二级引证文献5

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部