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多目标非脆弱鲁棒控制器在飞行控制系统中的应用 被引量：2

Application on Multi-Object Non-Fragile Robust Controller for Flight Control System
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摘要 针对飞行控制系统中存在的多种不确定性,提出了飞行控制系统的多目标非脆弱鲁棒控制器的控制方法。由系统的H2性能、H∞性能、区域极点配置和保性能控制四种控制目标,用线性矩阵不等式(LMI)法导出多目标鲁棒状态反馈控制器的存在条件,同时考虑了飞行控制系统中控制器增益的加性摄动,设计的控制器实现了系统的四种性能指标优化。仿真实验结果表明:该控制方法有较强的鲁棒性。 According to the multiply uncertainness in the flight control system, the multi-object non-fragile robust controller was proposed in this paper. From the four control objectives that were H2 performance, H∞ performance, regional pole placement and robust guaranteed cost control, the existing conditions of the multi-object robustness state feedback controller were deduced by linear matrix inequality （LMI） approach. Also, the designed controller optimized the four performances were realized when the gain variation of controller in fight control system was in consideration. The simulation results showed that this method had strong robustness.
作者 黄宜庆 黄友锐 魏圆圆 田一鸣
机构地区 安徽理工大学电气与信息工程学院 中国科学院合肥智能机械研究所
出处 《上海航天》 2010年第2期34-37,64,共5页 Aerospace Shanghai
关键词 飞行控制系统 非脆弱鲁棒控制器 H2控制 H∞控制 区域极点配置 保性能控制 线性矩阵不等式 Flight control system Non-fragile robust controller H2 control H∞ control Regional pole placement Guaranteed cost control Linear matrix inequality
分类号 V249.1 [航空宇航科学与技术—飞行器设计]
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参考文献10

二级参考文献34

  • 1[2]Kee L H,Bhattacharyya S P.Robust,fragile or optimal.IEEE Trans Automat Control,1997;42(8):1098-1105
  • 2[3]Yee J S,Wang J L.Yang G H.An LMI approachto no-fragilegoaranteed cost control of uncertain discrete time-delay systems.Asian Journal of Control,2001;3(3):226-233
  • 3[1]XU S Y,DOOREN P V,STEFAN R.Robust Stability and Stabilization for Singular Systems with State Delay and Parameter Uncertainty.IEEE Trans[J].Aautomatic Control,2002,47 (7):1 122-1 128.
  • 4[2]SU N J,SU H Y,CHU J.Delay-Dependent Robust H∞ Control for Uncertain Time-Delay Systems[J].IEEE Proc Control Theory Appl,2003,150 (5):489-492.
  • 5[3]KEEL L H,BHATTACHARYYA S P.Robust Fragile or Optimal[J].IEEE Trans on Automatic Control.1997,42 (8):1 098-1 105.
  • 6[5]YANG G H,WANG J L.Non-fragile H∞ Control for Linear Systems with Multiplicative Gain Variations[J].Automatica,2001,37 (5):727-737.
  • 7[6]CHANG S S L,PENG T K C.Adaptive Guaranteed Cost Control of Systems with Uncertain Parameters[J].IEEE Trans on Automatic Control,1972,17 (4):474-483.
  • 8Famularo D, Abclal!sh C T, Jadbabais A, et al. Robust nonfragile LQ controllers: the static state feedback case[A]. Proc American Control Conference[C]. Philadelphia: [s.n.], 1998. 1109- 1113.
  • 9Yang G H, Wang J L.Robust non - fragile Kalman filtering for uncertain linear systems with estimator gain uncertainty[J]. IEEE Trans Automatic Control, 2001, 46(2) : 343 - 348.
  • 10Xie L, Fu M,de Souza C E. H.control and quadratic stabilization of systems with parameter uncertainty via output feedback[J].IEEE Trans Automat Control, 1992, 37(8) :1253 - 1256.

共引文献7

同被引文献24

  • 1李正强,张怡哲,宋述杰,邓建华.非线性结构自适应模型逆飞行控制律设计研究[J].西北工业大学学报,2009,27(4):471-476. 被引量：2
  • 2陈谋,姜长生,吴庆宪.基于多模型方法的全包络鲁棒飞行控制器设计[J].航空学报,2006,27(3):486-492. 被引量：15
  • 3Hedrick J K, Gopalswamy S.Nonlinear flight control design via sliding methods[J].Joumal of Guidance, Control and Dynamics, 1990,13(5): 850-858.
  • 4Adams R J, Banda S S.Robust flight control design using dynamic inversion and structured singular value synthesis[J].IEEE Transactions on Control Systems Technology, 1993,1 (2) : 80-92.
  • 5Yang C D, Kung C C.Nonlinear H∞ flight control of general six-degree-of-freedom motions[J].Journal of Guidance, Control and Dynamics,2000,23(2) :278-288.
  • 6Wang Q, Stcngcl R F.Robust nonlinear flight control of a high-performance aircraft[J].IEEE Transactions on Control Systems Technology, 2005,13 (1) : 15-26.
  • 7Chen M, Ge S S, Ren B.Robust attitude control of helicopters with actuator dynamics using neural networks[J].IET Control Theory and Applications, 2010,4(12) : 2837-2854.
  • 8Hedrick J K, Gopalswamy S. Nonlinear flight control design via sliding methods [ J ]. Journal of Guidance, Control and Dynamics, 1990,13 (5) : 850 - 858.
  • 9Adams R J, Banda S S. Robust flight control design using dynamic inversion and structured singular value synthesis [ J ]. IEEE Transactions on Control Systems Technology, 1993,1 (2) :80 -92.
  • 10Yang C D, Kung C C. Nonlinear H∞ flight control of general six-degree-of-freedom motions [ J ]. Journal of Guidance, Control and Dynamics ,2000,23 (2) :278 - 288.

引证文献2

二级引证文献10

上海航天
2010年 第2期

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