Knowledge discovery from communication network alarm databases

The technique of Knowlege Discovery in Databases (KDD) to learn valuable knowledge hidden in network alarm databases is introduced. To get such knowledge, we propose an efficient method based on sliding windows (named as Slidwin) to discover different episode rules from time squential alarm data. The experimental results show that given different thresholds parameters, large amount of different rules could be discovered quickly. Foundation item: Supported by the National 863 High-Tech Project (863-306-Z705-02) and National Natural Science Foundation of China (69896240) Biography: Wang Xi-miao (1973-), female, Ph. D. candidate. Research interests: network management and information processing.     

Sliding mesh algorithm for CFD analysis of helicopter rotor–fuselage aerodynamics

The study of rotor–fuselage interactional aerodynamics is central to the design and performance analysis of helicopters. However, regardless of its significance, rotor–fuselage aerodynamics has so far been addressed by very few authors. This is mainly due to the difficulties associated with both experimental and computational techniques when such complex configurations, rich in flow physics, are considered. In view of the above, the objective of this study is to develop computational tools suitable for rotor–fuselage engineering analysis based on computational fluid dynamics (CFD). To account for the relative motion between the fuselage and the rotor blades, the concept of sliding meshes is introduced. A sliding surface forms a boundary between a CFD mesh around the fuselage and a rotor‐fixed CFD mesh which rotates to account for the movement of the rotor. The sliding surface allows communication between meshes. Meshes adjacent to the sliding surface do not necessarily have matching nodes or even the same number of cell faces. This poses a problem of interpolation, which should not introduce numerical artefacts in the solution and should have minimal effects on the overall solution quality. As an additional objective, the employed sliding mesh algorithms should have small CPU overhead. The sliding mesh methods developed for this work are demonstrated for both simple and complex cases with emphasis placed on the presentation of the inner workings of the developed algorithms. Copyright © 2008 John Wiley & Sons, Ltd.     

利用Backstepping法设计机械手跟踪控制器

针对机械手跟踪控制问题提出了一种新的设计方法 .此法应用 Bachstepping方法的思想 ,保证系统稳定的条件下 ,同时设计控制规律和观测器 ,并用数字仿真对设计法的正确性进行了验证     

血药浓度最优控制系统的状态观测器设计

为使血药浓度最优控制律成为现实可行的、有效的控制手段。设计了结构简单的全维状态观测器。     

拉索支座减隔震桥梁自适应推倒分析方法

以拉索支座减隔震桥梁为研究对象,提出了自适应推倒分析方法(AMPP),对比多模态推倒分析方法(MPA)和一阶模态推倒分析方法(PO-1),研究AMPP方法应用于这类桥梁抗震性能评估的可行性及效果.结果表明:推倒分析方法可以成功应用于拉索支座减隔震桥梁的抗震性能评估,AMPP方法对关键参数的计算精度高于一阶模态推倒分析和多模态推倒分析,但多模态推倒方法对下部构件的内力评估精度较好.     

车辆质心侧偏角估计算法设计与对比分析

车辆质心侧偏角是描述车辆侧向运动状态的重要变量之一,同时也很难准确估计.为此设计了基于运动学的直接积分法,基于扩展卡尔曼滤波的质心侧偏角估计算法和基于广义龙贝格观测器的质心侧偏角估计算法.对信号引入一定强度的噪声,通过多种典型工况对质心侧偏角估计算法进行调试与验证,分析不同算法的特点和工况适应性.直接积分法在长时间尺度下无可用性,但在极限工况下能较为快速地描述质心侧偏角变化趋势;卡尔曼滤波算法整体估计效果较好,但在一些动态工况存在估计偏差,且多为高估;龙贝格观测器算法在大部分工况都能获得良好效果,但在某些情况下存在估计偏差,且多为低估.     

车用乙醇汽油体积分数估计

为获得精确的乙醇体积分数,在发动机进气模型的基础上,设计了高增益观测器估计歧管压力,并对观测器误差进行了收敛性和稳定性分析.设计PI控制器对空燃比进行控制,使过量空气系数趋于理论值.利用PI控制器输出的燃油反馈信号,通过积分清零运算得出化学计量空燃比(Rs),根据Rs与乙醇体积分数的关系计算得出乙醇体积分数估计值.仿真结果表明:乙醇体积分数估计时间在2s以内,估计误差绝对值小于1%,满足汽车的排放性和经济性要求.     

过失速机动变指数趋近律UAS-SMC设计

针对常规指数趋近律单向辅助面滑模控制中存在的抖振问题, 提出了一种基于变指数趋近律的单向辅助面滑模控制方法。针对系统控制量变化时飞机模型发生跳变的问题, 进行T-S 模糊建模, 以保证非线性系统在控制区间上的平滑性; 在对UAS-SMC(Unidirectional Auxiliary Surfaces-Sliding Mode Control)方法进行分析的基础
上, 给出了一种变指数的趋近律; 结合飞机模型和变指数趋近律, 设计了基于变指数单向辅助面滑模控制器。仿真实验结果表明, 该控制策略能保证趋近过程快速性的同时在接近滑模面时能有效减少系统的抖振。     

基于模糊神经滑模观测器的永磁同步电机无传感器控制

为了解决传统滑模观测器的抖振问题,提出了一种用于永磁同步电机的模糊神经滑模观测器。分析了滑模增益对抖振的影响,并采用模糊神经网络动态调整滑模增益以改善抖振,利用李雅普诺夫函数证明了模糊神经网络观测器的稳定性。利用锁相环方法提取转子位置与速度信息,减小由高频噪声引起的误差。仿真结果表明:改进后的滑模观测器能够对永磁同步电机转子位置进行精确辨识,有效地抑制了抖振,实现了高性能的永磁同步电机无传感器控制。     

AMT重型越野车辆坡道起步改进控制策略

针对AMT重型越野车辆大坡道起步过程中离合器摩擦片磨损严重的问题,提出了坡道起步改进控制策略. 将坡道起步过程划分成4部分,结合改进前的离合器控制策略和大坡道起步数据,分别针对每一部分进行了减少滑摩功的分析. 在改进后的控制策略中,将离合器结合过程与发动机转速下降率进行闭环控制,防止因起步过快而造成发动机熄火. 以某AMT重型越野车辆为试验平台,重新设计了坡道起步过程中的离合器控制策略,编写了控制软件,并进行了不同大坡道的起步验证,取得了理想的效果.