基于T-S模糊模型的CNN混沌同步控制研究

研究了四元细胞神经网络(CNN)混沌系统的T-S模糊模型建立问题,用李雅谱诺夫法构建CNN混沌系统的同步控制器,并用遗传算法对控制参数进行优化,达到比较理想的同步效果.     

模糊时滞系统的稳定性

文章考虑了T-S模糊模型的指数稳定性和模糊观测器的设计问题,利用模糊观测器的状态反馈和矩阵不等式技巧,给出了闭环系统指数稳定的充分条件.     

Reliable fuzzy control with domain guaranteed cost for fuzzy systems with actuator failures

The reliable fuzzy control with guaranteed cost for T-S fuzzy systems with actuator failure is proposed in this paper. The cost function is a quadratic function with failure input. When the initial state of such systems is known, a design method of the reliable fuzzy controller with reliable guaranteed cost is presented, and the formula of the guaranteed cost is established. When the initial state of such systems is unknown but belongs to a known bounded closed domain, a notion of the reliable domain guaranteed cost (RDGC) for such systems is proposed. For two classes of initial state domain, polygon domain and ellipsoid domain, some design methods for reliable fuzzy controllers with the RDGC are provided. The efficiency of our design methods is finally verified by numerical design and simulation on the Rossler chaotic system.     

T-S模糊神经网络在冠心病智能诊断中的应用

 冠心病是一种最为常见的心血管疾病,近年来在中国的发病率与死亡率逐年升高,准确诊断和及时治疗是有效降低冠心病死亡率的主要措施。通过引入模糊系统的理论,在传统BP神经网络结构中加入了模糊层与模糊规则计算层,建立了T-S模糊神经网络模型。使用该模型对采集于克利夫兰诊所的297组数据进行分析预测,与传统BP神经网络预测结果对比显示,T-S模糊神经网络模型的平均准确率为82.93%,而传统BP神经网络的平均准确率为75.56%,表明T-S模糊神经网络模型在冠心病的智能诊断中具有较高的预测准确率。     

控制Lorenz系统的新方法

讨论Lorenz混沌系统的控制问题.首先将Lorenz系统用模糊T-S模型来表示,然后引入脉冲控制律,利用脉冲微分系统理论进行分析,得到了Lorenz系统的脉冲控制准则.根据该准则所设计的脉冲控制器,可以驱动受控Lorenz系统的轨线以指数衰减率收敛于平衡点.     

时滞非线性系统的模糊保性能控制

针对一类具有输入与状态时滞的参数不确定非线性系统,基于T-S模糊模型,讨论该系统的保性能控制问题.通过构造状态反馈控制器,提出了在给定的性能指标和控制律下,闭环系统是二次保性能稳定的充分条件,并以线性矩阵不等式(LM I)的形式表示,数值算例显示该设计方法是有效的.     

基于均匀设计的T-S建模方法

T-S模糊系统被广泛应用在基于数据的建模方法中.模糊规则作为T-S模糊系统的核心,是影响系统精度和泛化性能的重要因素,然而模糊规则数量的确定非常困难.考虑基于减聚类的规则生成方法中,聚类半径直接影响规则生成数量,采用均匀设计设定聚类半径,合理选择规则数量,简化了复杂多变量系统的建模问题.实例证明所提出基于均匀设计思想的聚类半径设定法简单易行,具有较好的实际应用价值,适合于复杂多变量系统的建模应用.     

Scattering of Tollmien-Schlichting waves by localized roughness in transonic boundary layers

The laminar-turbulent transition in boundary-layer flows is often affected by wall imperfections, because the latter may interact with either the freestream perturbations or the oncoming boundary-layer instability modes, leading to a modification of the accumulation of the normal modes. The present paper particularly focuses on the latter mechanism in a transonic boundary layer, namely, the effect of a two-dimensional(2 D) roughness element on the oncoming Tollmien-Schlichting(T-S) modes when they propagate through the region of the rapid mean-flow distortion induced by the roughness. The wave scattering is analyzed by adapting the local scattering theory developed for subsonic boundary layers(WU, X. S. and DONG, M. A local scattering theory for the effects of isolated roughness on boundary-layer instability and transition: transmission coefficient as an eigenvalue. Journal of Fluid Mechanics, 794, 68–108(2006)) to the transonic regime, and a transmission coefficient is introduced to characterize the effect of the roughness. In the sub-transonic regime, in which the Mach number is close to, but less than, 1, the scattering system reduces to an eigenvalue problem with the transmission coefficient being the eigenvalue; while in the super-transonic regime, in which the Mach number is slightly greater than 1, the scattering system becomes a high-dimensional group of linear equations with the transmission coefficient being solved afterward. In the largeReynolds-number asymptotic theory, the K′arm′an-Guderley parameter is introduced to quantify the effect of the Mach number. A systematical parametric study is carried out,and the dependence of the transmission coefficient on the roughness shape, the frequency of the oncoming mode, and the K′arm′an-Guderley parameter is provided.     

基于三角形模糊数的非线性T-S模糊系统的峰值点和分量半径优化

单值模糊器是将高维空间中一个实值点映射成该空间上的一个单值模糊集,在构造非线性T-S模糊系统时不仅可克服输入变量的噪声问题,而且能减少模糊推理机设计中的计算量.首先,基于分片线性函数和单值模糊器给出了非线性T-S模糊系统模型;并依据广义三角形的重心坐标公式,对等距剖分论域中的峰值点和分量半径等参数进行了优化;最后,通过模拟实例对系统进行了验证,得到优化后的非线性T-S模糊系统确实有更好的逼近效果.     

A numerical investigation of the evolution of 2-D disturbances in hypersonic boundary layers and the effect on the flow structure due to the existence of shocklets

The evolution of 2-D disturbances in hypersonic boundary layer with Mach number 6,8, and 10 was investigated numerically by three different numerical schemes. At the entrance, second mode T-S waves with different amplitudes were introduced, and the relation between the Mach number and the amplitude of the disturbance when shocklets started to appear was investigated. By comparing the disturbance velocity profiles with those provided by linear stability theory, the effects of shocklets on flow structures were also investigated.