Hammerstein系统遗忘因子有限窗口分解辨识

提出一种带遗忘因子和分解辨识策略的有限数据窗口递归最小二乘Hammerstein系统辨识方法。针对Hammerstein系统具有耦合参数的问题,将Hammerstein系统分解为2个子系统：一个子系统包含线性子系统参数,另一个子系统包含非线性子系统参数;提出一种基于遗忘因子的有限窗口递归最小二乘方法对分解模型进行在线递归估计;仿真示例验证了所提算法能够快速跟踪参数,实现对Hammerstein系统的精确辨识。     

基于残差卷积自注意力神经网络的铝电解过热度识别方法

过热度是反映铝电解槽当前生产效率的重要指标,由于过热度难以在线实时测量,本文提出一种基于残差卷积自注意力神经网络的过热度识别方法.针对铝电解生产过程数据为时间序列数据且具有多源异构特性,设计异构数据的同构表示方法.在此基础上建立残差卷积自注意力神经网络模型以提取同构时间序列数据的全局与局部特征.针对过热度数据标签少且类别分布不均匀问题,采用基于自动编码器的无监督预训练方法与加权交叉熵损失函数以提高过热度识别任务的性能.在基准数据集上进行仿真对比实验以验证本文所提方法的有效性,然后在只包含少量不平衡标签的铝电解过热度数据集上进行实验验证,结果表明本文构建的过热度识别模型相较与其他现有模型不仅提高了过热度识别准确率,而且在训练样本较少时保证了模型的泛化能力.     

基于机器视觉的车辆时空参数识别

车辆荷载信息是分析桥梁受力和性能评估的重要依据,其中车辆时空信息是准确识别车辆荷载的关键参数。考虑到传统在桥面埋设传感器的方法影响交通、破坏路面,提出了一种基于机器视觉技术的车辆荷载时空参数识别方法,包括车辆的横向定位、车速、车轴数、轴距的识别。基于正面拍摄视频,采用背景差分法来实现车辆检测,进一步通过车牌识别确定车辆在图像中的位置,然后根据车牌与车道线距离来实现车辆横向定位。基于侧面拍摄视频,采用图像标定方法,结合已知长度的辅助检测线来获取车辆的轴距、轴数、车速等车辆参数。通过试验室模型试验和现场试验验证了提出的方法。结果表明,现场试验中车辆横向定位和车速的最大误差分别为2.42%和2.67%,轴距的平均误差为1.63%,识别结果可以为更多其他车辆参数如轴重和总重的识别提供重要的技术支撑。     

蛋白质组学技术在动物科学中的研究进展

蛋白质组学在后基因组时代以其独特的角度和重要的作用已成为生命科学领域研究的热点内容。动物科学作为生命科学的一个重要分支,其相关研究对人类的生活有着重要意义。为了系统地了解和展望蛋白质组学技术在动物科学中的研究进展,综述了蛋白质组学的概念及其相关技术,归纳和评析了近年来蛋白质组学在动物繁殖、营养、遗传育种和疾病防治方面的研究现状。     

耐碳青霉烯酶肺炎克雷伯菌的分离鉴定及生物学特性分析

以临床尿路感染患者尿液为研究对象,通过分离培养及16s rDNA进行肺炎克雷伯菌的分离鉴定;采用Kirby-Bauer纸片法进行药敏实验,并对分离株进行碳青霉烯酶表型筛选;通过PCR检测常见的碳青霉烯酶耐药基因、荚膜血清型和毒力基因分布情况;对分离的肺炎克雷伯菌株进行了生物被膜形成能力及其对小鼠致病力的分析。本研究从采取的86例尿液标本中分离检出11株耐碳青霉烯酶肺炎克雷伯菌,分离率为12.79%。耐碳青霉烯酶基因PCR检测结果显示,blaNDM、blaVIM、blaIMP和blaKPC基因在分离株中均呈现不同程度的分布。耐药性分析发现11株肺炎克雷伯菌对氨苄西林耐药率为90.91%,对头孢噻肟耐药率为63.64%,对链霉素、庆大霉素、氯霉素和诺氟沙星的耐药率较低。耐碳青霉烯类肺炎克雷伯菌荚膜分型结果显示,分离的11株细菌中10株均为强毒力型菌株（90.9%）,其中K57血清型4株（36.4%）,K1血清型1株（9.1%）,K2血清型1株（9.1%）,K5血清型1株（9.1%）,K20血清型3株（27.3%）,提示该批分离株具有较强的致病力。此外,毒力因子分布结果显示,其毒力因子rmpA（54.5%）、Aerobactin F（54.5%）在菌株中分布较为广泛。生物被膜形成能力检测及小鼠致病性试验结果显示,9株分离株均有较强的生物被膜形成能力,菌株致病力可能与荚膜血清型及生物被膜形成能力相关。综上所述,临床分离的致尿路感染病原肺炎克雷伯菌呈现多重耐药特征,强毒力菌株以K57荚膜型为主,K1、K2均有分布,提示对尿路感染病原应加强耐药监测,合理使用抗菌药物,有效防控多重耐药和强毒力菌株的感染与流行。     

Real-time onboard wind and windshear determination,part 2: Detection

This paper is concerned with windshear detection in connection with real-time wind identification (Ref. 1). It presents a comparative evaluation of two techniques, one based on the shear/downdraft factor and one based on the wind difference index. The comparison is done with reference to a particular microburst, that which caused the 1985 crash of Flight Delta 191 at Dallas-Fort Worth International Airport.The shear/downdraft factor has the merit of combining the effects of the shear and the downdraft into a single entity. However, its effectiveness is hampered by the fact that, in a real situation, the windshear is accompanied by free-stream turbulence, which tends to blur the resulting signal. In turn, this results in undesirable nuisance warnings if the magnitude of the shear factor due to free-stream turbulence is temporarily larger than that due to true windshear. Therefore, proper filtering is necessary prior to using the shear/downdraft factor in detection and guidance. One effective way for achieving this goal is to average the shear/downdraft factor over a specified time interval . The effect of on the average shear/downdraft factor is studied.     

Real-time onboard wind and windshear determination,part 1: Identification

Standard wind identification techniques employed in the analysis of aircraft accidents are post-facto techniques; they are processed after the event has taken place and are based on the complete time histories of the DFDR/ATCR data along the entire trajectory. By contrast, real-time wind identification techniques are processed while the event is taking place; they are based solely on the knowledge of the preceding time histories of the DFDR/ATCR data.In this paper, a real-time wind identification technique is developed. First, a 3D-kinematic approach is employed in connection with the DFDR/ATCR data covering the time interval preceding the present time instant. The aircraft position, inertial velocity, and accelerometer bias are determined by matching the flight trajectory computed from the DFDR data with the flight trajectory available from the ATCR data. This leads to a least-square problem, which is solved analytically every seconds, with / small.With the inertial velocity and accelerometer bias known, an extrapolation process takes place so as to predict the inertial velocity profile over the subsequent -subinterval. At the end of this subinterval, the extrapolated inertial velocity and the newly identified inertial velocity are statistically reconciled and smoothed. Then, the process of identification, extrapolation, reconciliation, and smoothing is repeated. Subsequently, the wind is computed as the difference between the inertial velocity and the airspeed, which is available from the DFDR data. With the wind identified, windshear detection can take place (Ref. 1).As an example, the real-time wind identification technique is applied to Flight Delta 191, which crashed at Dallas-Fort Worth International Airport on August 2, 1985. The numerical results show that the wind obtained via real-time identification is qualitatively and quantitatively close to the wind obtained via standard identification. This being the case, it is felt that real-time wind identification can be useful in windhsear detection and guidance, above all if the shear/downdraft factor signal is replaced by the wind difference signal (Ref. 1).This paper and its companion (Ref. 1) are based on Refs. 2–4.This research was supported by the Aviation Research and Education Foundation and by Texas Advanced Technology Program, Grant No. TATP-003604020.     

Fastiterative methods for least squares estimations

Least squares estimations have been used extensively in many applications, e.g. system identification and signal prediction. When the stochastic process is stationary, the least squares estimators can be found by solving a Toeplitz or near-Toeplitz matrix system depending on the knowledge of the data statistics. In this paper, we employ the preconditioned conjugate gradient method with circulant preconditioners to solve such systems. Our proposed circulant preconditioners are derived from the spectral property of the given stationary process. In the case where the spectral density functions() of the process is known, we prove that ifs() is a positive continuous function, then the spectrum of the preconditioned system will be clustered around 1 and the method converges superlinearly. However, if the statistics of the process is unknown, then we prove that with probability 1, the spectrum of the preconditioned system is still clustered around 1 provided that large data samples are taken. For finite impulse response (FIR) system identification problems, our numerical results show that annth order least squares estimator can usually be obtained inO(n logn) operations whenO(n) data samples are used. Finally, we remark that our algorithm can be modified to suit the applications of recursive least squares computations with the proper use of sliding window method arising in signal processing applications.Research supported in part by HKRGC grant no. 221600070, ONR contract no. N00014-90-J-1695 and DOE grant no. DE-FG03-87ER25037.     

光伏模组积灰与阴影特性分析及识别方法

针对光伏模组积灰与阴影特性识别问题,详细分析了积灰和阴影的光伏特性曲线差异,揭示了阴影光伏曲线的拐点时变特性。提出由特性曲线的拐点数量及电流电压特性条件共同构成训练模型的输入特征量,基于CatBoost算法训练积灰和阴影识别模型。最后,利用光伏模组实测数据对CatBoost算法、ID3和GA-BP算法训练出的识别模型进行性能分析和对比测试,结果表明基于CatBoost训练出的识别模型输入量区分性强、诊断精度高,极具工程应用价值。