基于T-S模糊模型的非线性时滞系统H∞滤波器设计

基于Takagi-Sugeno模糊模型, 研究了时变时滞非线性模糊系统的滤波器设计方法. 通过构造改进的Lyapunov泛函, 结合自由权矩阵与矩阵解耦方法, 提出模糊H∞滤波器存在充分条件. 此充分条件较已有文献中类似条件具有更低的保守性. 并给出示例说明了所给出方法的有效性.     

基于秘密共享模数的一般性多方求逆协议

Catalano、Gennaro和Halevi提出了一个实用的基于秘密共享模数的分布式求逆协议,然而他们仅仅考虑了门限敌手结构的情况.文中考虑了一般敌手结构的情况,针对半诚实敌手和恶意敌手,利用Damgard和Thorbek提出的线性整数秘密共享方案,分别构造了一个多方模求逆协议.该协议在敌手结构是Q2(对应Q3以及强RSA假设)的条件下针对半诚实(对应恶意)敌手是安全的.该协议是Catalano等人方案的一个推广,可以用来分布式地计算RSA私钥以及构造标准模型下安全的分布式Gennaro-Halevi-Rabin、Cramer-Shoup和Mames-Joye签名方案.另外,文中的构造方法也是对环上的安全多方协议构造方法的一个有力补充.     

PAC在气体流量标准装置中的应用

为实现气体流量计检定测试的准确性、提高试验系统的自动化程序和可靠性,在气体流量标准装置中采用可编程自动化控制器PAC控制方式.考虑到测试条件应接近流量计的真实工作环境这一因素,设计了气源系统精确调节方法及其相应程序.经过实践证明,基于PAC的变频调速技术在气体流量检定测试过程中的应用效果良好,满足流量计检定要求.     

核判决分析及其在表情识别中的应用

提出了一种基于核判决分析(KDA)的人脸表情识别方法.与传统的线性特征提取方法线性判决分析(LDA)不同,针对非线性问题,KDA通过引入核函数进行非线性投影以提取表情特征,克服了LDA算法用于人脸表情识别时存在的问题.基于CED-WYU(1.0)和JAFFE两个表情数据库的识别结果表明, 基于核判决分析KDA的特征提取方法能有效地提高识别率.     

Improved exponential stability criteria for uncertain neutral system with nonlinear parameter perturbations

This paper investigates the problem of robust exponential stability for neutral systems with time-varying delays and nonlinear perturbations. Based on a novel Lyapunov functional approach and linear matrix inequality technique, a new delay-dependent stability condition is derived. Since the model transformation and bounding techniques for cross terms are avoided, the criteria proposed in this paper are less conservative than some previous approaches by using the free-weighting matrices. One numerical example is presented to illustrate the effectiveness of the proposed results.     

Robust active suspension design subject to vehicle inertial parameter variations

This paper presents an approach in designing a robust controller for vehicle suspensions considering changes in vehicle inertial properties. A four-degree-of-freedom half-car model with active suspension is studied in this paper, and three main performance requirements are considered. Among these requirements, the ride comfort performance is optimized by minimizing the H∞ norm of the transfer function from the road disturbance to the sprung mass acceleration, while the road holding performance and the suspension deflection limitation are guaranteed by constraining the generalized H2 (GH2) norms of the transfer functions from the road disturbance to the dynamic tyre load and the suspension deflection to be less than their hard limits, respectively. At the same time, the controller saturation problem is considered by constraining its peak response output to be less than a given limit using the GH2 norm as well. By solving the finite number of linear matrix inequalities (LMIs) with the minimization optimization procedure, the controller gains, which are dependent on the time-varying inertial parameters, can be obtained. Numerical simulations on both frequency and bump responses show that the designed parameter-dependent controller can achieve better active suspension performance compared with the passive suspension in spite of the variations of inertial parameters.     

Delay-dependent stability analysis for Markovian jump systems with interval time-varying-delays

This paper proposes improved stochastic stability conditions for Markovian jump systems with interval time-varying delays. In terms of linear matrix inequalities (LMIs), less conservative delay-range-dependent stability conditions for Markovian jump systems are proposed by constructing a different Lyapunov-Krasovskii function. The resulting criteria have advantages over some previous ones in that they involve fewer matrix variables but have less conservatism. Numerical examples are provided to demonstrate the efficiency and reduced conservatism of the results in this paper.     

基于CCD的垂线坐标仪的设计

针对矿井井壁变形引起的径向位移测量问题,提出了一种基于CCD的垂线坐标仪的设计方案,给出了垂线坐标仪的结构及其在井壁变形监测系统中的布置,详细介绍了垂线坐标仪的软、硬件设计。该垂线坐标仪利用CCD采集光信号并将其转换为视频信号,采用LPC932对采集的视频信号进行二值化处理及计数,并将处理结果发送至地面计算机进行分析,从而得到矿井井壁变形引起的径向位移量。测试结果验证了该垂线坐标仪的稳定性和精确性。     

直升机鲁棒保性能控制律设计

考虑直升机在飞行包线内模型参数的变化及不确定性影响,设计了鲁棒保性能控制律;根据直升机一个标称状态点构造出了参数不确定性矩阵,利用Lyapunov稳定性定理和线性矩阵不等式方法给出了控制器存在的充分条件及参数化设计方法,进行直升机三轴姿态稳定保性能控制律的设计;仿真结果表明,所设计的控制器满足三轴姿态稳定要求且具有很好的鲁棒性。