基于智能集成架构的时间序列数据挖掘算法研究

针对单一算法在处理复杂时间序列数据时存在缺陷以致无法挖掘全部信息的问题,提出了智能集成架构,给出了4种集成结构,并分析了它们的适用情况。针对一类随机噪声干扰的时间序列数据,采用并联嵌套建模结构,提出嵌套双种群粒子群算法的自回归滑动平均(ARMA)模型,用于挖掘数据中的随机性趋势;提出基于概率密度控制(PDF)的最小二乘支持向量机(LSSVM),用于挖掘数据中的确定性趋势,两种模型并联补集成实现对数据信息的充分挖掘。通过一组实验验证了所提方法的效果。     

基于Attention的AIS数据段相似性搜索模型

自动识别系统(Automatic Identification System,AIS)数据中蕴含着与船舶交通相关的时间序列信息.基于AIS数据段的相似性搜索也成为智能船运领域的研究热点.AIS数据属于多维时间序列数据,传统的多维数据序列相似性搜索方法通过将原始数据进行降维,并在降维后的数据空间进行时序数据的相似性搜索....     

双向时空连续性轨迹片段关联的目标跟踪方法

提出一种使用双向时空连续性关联轨迹片段的目标跟踪方法.首先对检测结果进行简单的帧间匹配关联,生成可靠的轨迹片段;然后对每个轨迹片段通过卡尔曼滤波以及有权重的均值法分别计算修正轨迹片段的速度、位置与颜色特征;最后通过计算轨迹片段之间的双向时空连续性迭代关联,找到最符合时空连续性的轨迹片段关联.实验证明本文方法可以有效解决...     

认知无线网络中不同场景的动态频谱聚合算法

在认知无线电网络中,不连续的频谱片段可以通过频谱聚合来满足认知用户的用频需求。常用的频谱聚合算法有具有聚合能力的频谱分配算法、最大满足算法和最小切换算法等。文章在这几种算法的基础上提出了一种能够预测高级用户出现概率的方法,从而减少网络开销;对于用频需求较大的情况,提出了折中算法和片段最大化算法,增加了可支持的用户数量,并减少了网络开销。仿真结果表明,上述算法具有较好的效果。     

多平台纯方位信息融合结构及关联估计联合优化模型

在多平台纯方位信息融合中,存在多平台的方位关联和单平台的参数估计(或目标定位)困难,因为两者相互依赖和制约。造成相对不同平台的方位不能进行时间空间对准、虚假目标不能消除。为此,提出了一种分布式信息融合结构,并建立了相应的数据互联与参数估计联合优化模型。在这种结构和模型中,首先由各平台对本地传感器探测的纯方位信息完成融合并输出方位序列,然后在融合中心按分层节点对方位序列的数据互联与参数估计进行联合优化处理,每个融合节点仅处理两个平台信息,最后节点输出融合结果。仿真计算结果表明,这种优化模型是解决关联和估计问题的一个有效方法,可以提高多平台纯方位信息融合的性能。     

计划中的时序偏好表示和非单调推理

针对行动序列计划中的时序偏好问题开展研究,重点关注时序偏好集合内部存在不一致性时完成行动计划的方法。论文的难点和创新点体现在两个方面。针对时序偏好的表示问题,建立了一种二元描述结构,能够实现对时序约束和时序偏好的归一化描述。使用计算辩论技术建立推理框架,用以排除约束/偏好集合中的冲突关系,获得具有最大一致性的约束/偏好子集。在此基础上建立了一种新的计划生成策略,通过映射的方法得到行动序列片段,组合这些片段后形成完整的行动序列计划。通过实例验证了方法的可行性。     

基于AIS的对海雷达多目标联合误差估计方法

提出了一种基于AIS的对海警戒雷达多目标联合误差估计方法,该方法以高精度AIS提供的目标信息为目标真值,对雷达进行误差估计。利用系统积累的多目标航迹信息,首先进行目标粗关联,将航迹信息进行时空对准后产生误差序列,通过单目标误差序列统计信息进行异常值的筛选,再通过多目标误差序列进行错误关联目标的检验,最终对剩余误差序列进行误差估计。通过实测数据和实际应用证明,该方法估计的雷达误差较准确,用估计结果对雷达误差进行校准后可有效减小对海雷达的系统误差。     

小粒野生稻可转化人工染色体文库初步构建及筛选

以小粒野生稻核DNA为材料构建了-个可转化人工染色体文库,获得了5000个克隆,平均插入片段约45kb.稳定性检测结果表明,小粒野生稻基因组DNA能够在TAC载体中稳定存在.基于已克隆抗性基因的保守序列设计探针,利用菌落杂交的方法,对文库进行筛选.结果表明,该文库可以用于抗性基因的筛选.     

基于节约训练时隙的多中继协作通信分段信道估计

在多中继放大转发协作通信系统中,针对分段信道估计时需要增加额外的时隙来发送训练序列的问题,提出一种节约训练时隙的分段信道估计方法。该方法结合预编码技术和半盲信道估计技术,在源节点对数据序列进行预编码,使其与训练序列正交后叠加,在中继节点进行预编码,使不同中继间的训练序列彼此正交,进而估计出每条链路的信道信息值。仿真结果表明,提出的方法只需占用1个训练时隙,并可有效获取S→R链路和R→D链路每段链路的信道信息,且R→D链路的平均MSE估计性能比S→R链路大约有5 dB的优势,提高了系统的传输效率。     

改进型JDL模型在武警部队院校信息化建设中的构建

在武警部队院校的网络信息化水平迅速发展的今天,由于各功能模块缺少统一的接口规范和能够协调各部门信息共享的机制,使得建成的各个功能模块之间无法共享信息,造成了数据库中信息的大量冗余和重复。结合数据融合技术的基本原理、发展现状和应用前景,对数据融合技术进行了介绍;针对武警院校信息融合的需求,提出了改进型JDL模型,分析了武警院校信息融合网络的服务架构层次,对信息融合网络中的核心问题信息共享、接口规范、数据融合进行了研究;利用模块化设计的思路,对原型系统进行了分析,对实验数据进行了重组,并提出了数据优化方案。     

直接免疫PCR方法的建立

免疫PCR基本原理与ELISA相似,即用一段可扩增的DNA分子代替ELISA中酶放大检出信号,建立了直接免疫PCR的检测蓖麻毒素技术,实验结果表明,其灵敏度达1pg／ml,比ELISA方法灵敏度高10^3倍.     

一种时空数据流中范围聚集查询共享策略

根据查询谓词的相似性来实现计算共享是数据流查询优化的主要策略之一,主要针对时空数据流中基于滑动窗口的范围聚集问题进行查询优化,采用时间片段和空间片段分别描述滑动窗口之间和空间范围谓词之间的重叠。提出基于时空分片技术将时空数据流元组分成互不重叠的时空片段。范围聚集查询首先基于时空片段生成中间结果,然后根据查询条件与时空片段的映射关系生成查询结果。实验表明,提出的时空分片策略能大大提高时空数据流中范围聚集查询的性能。     

Parametric study of single confined fragment launch explosive device

In this article, parametric study of single confined fragment launch device was carried out. The configuration proposed was further studied to derive the empirical relationship for effect of fragment size, charge size, confinement thickness on fragment velocity. The simulations were carried out using ANSYS-AUTODYNE explicit solver. Fragment velocities were estimated as a function of different parametric combinations of explosive quantities, charge length to diameter ratio, fragment height to diameter ratio, confinement thickness, fragment material and fragment mass. The data was further converted to charge to metal ratio under fragment and confinement. It was observed that, increase in confinement thickness, charge quantity and decrease in fragment height increases the fragment velocity. It is also noted that, charge to metal mass ratio under fragment significantly affects the fragment velocity. At the end, an empirical relationship for fragment velocity interms of all these parameters was established. Using these relations, two velocities 1831.92 m/s and 2523.9 m/s required for NATO STANAG 4496 IM test were estimated. The design parameters for these velocities are presented. Also, the results estimated using the empirical relationship has been compared with published experimental data. Error in the predicted velocities is within the acceptable range. The empirical relationship proposed will be useful for finalization of design of the fragment launch device.     

Ricochet quantification using a multiple sensor approach

This study investigates the ricochet behaviour of three different small-arms projectile types using a novel ricochet measuring device.The results can be used to estimate the danger potential of ricochets on shooting ranges.A ricochet is the change of direction and velocity of a projectile after impacting an oblique surface.This impact produces strong vibrations on a rigid plate.During this impact,flexural waves travel radially outwards from the point of impact.These waves are used to determine the properties of the impactor with accelerometers situated on the target surface.With the use of two measurement plates,one can produce a ricochet and detect the velocity at the same time.Accelerometers are suitable for accurate momentum measurements of single impacts.However,depending upon strike velocity and the impact angle,a ricochet can separate in multiple fragments after being deflected.From the operational safety perspective,these fragments need to be detected,as well.The approach of a coupled sensor concept was chosen to solve this problem.Thermographic sensors were additionally used to visualise the heat which is produced after pene-trating a rubber layer pasted in front of the steel target plate.With this approach one was able to detect the position of impact.The investigations showed that the measurement system performance is better with a multiple sensor design,which includes accelerometers for the velocity,impact strength and partly the position measurement,while the thermographic sensor was used for the position measurement and partly the momentum measurement.The investigated ammunition showed plausible fragmentation behaviour,and the results can already be used to estimate the danger potential of different ammunition types.Frangible projectiles fragment to small particles already after being deflected under a small angle.However,Full Metal Jacket projectiles with or without a steel core do not fragment under angles which are less than 5°.The objective of the paper is to demonstrate the possibility of measuring the complex ricochet me-chanics of small projectiles using standard accelerometers with the adequate signal processing approach.This measuring system is supported by an off the shelf thermographic camera.     

Numerical simulation study on penetration performance of depleted Uranium (DU) alloy fragments

Due to its high strength, high density, high hardness and good penetration capabilities, Depleted ura-nium alloys have already shined in armor-piercing projectiles. There should also be a lot of room for improvement in the application of fragment killing elements. Therefore, regarding the performance of the depleted uranium alloy to penetrate the target plate, further investigation is needed to analyze its advantages and disadvantages compared to tungsten alloy. To study the difference in penetration per-formance between depleted uranium alloy and tungsten alloy fragments,firstly, a theoretical analysis of the adiabatic shear sensitivity of DU and tungsten alloys was given from the perspective of material constitutive model. Then, taking the cylindrical fragment penetration target as the research object, the penetration process and velocity characteristics of the steel target plates penetrated by DU alloy frag-ment and tungsten alloy fragment were compared and analyzed, by using finite element software ANSYS/LS-DYNA and Lagrange algorithm. Lastly, the influence of different postures when impacting target and different fragment shapes on the penetration results is carried out in the research. The results show that in the penetration process of the DU and tungsten alloy fragments, the self-sharpening properties of the DU alloy can make the fragment head sharper and the penetrating ability enhance. Under the same conditions, the penetration capability of cylindrical fragment impacting target in vertical posture is better than that in horizontal posture, and the penetration capability of the spherical fragment is slightly better than that of cylindrical fragment.     

Effect of the end cap on the fragment velocity distribution of a cylindrical cased charge

The prediction of the fragment velocity distribution of a cylindrical cased charge with end caps is one of the key issues to assess the damage efficiency of the warhead. However, limited work has been con-ducted to predict the fragment velocity distributions along the axis of cylindrical cased charges with end caps. This paper presents a study of the velocity distribution of fragments caused by the explosion of a cylindrical cased charge with end caps. The fragment velocity distribution and the end cap velocity were determined by an X-ray radiography method, and the axial fragment distribution was determined by witness plates. It was found that the velocities of fragments, especially near the edge, were increased when the end caps were added, and the position of maximum velocity is closer to the non-detonation end. The fragment velocities were increased, and the fragment projection range was decreased with the increase of the thickness of the end cap. A formula for fragment velocity distributions of a cylindrical cased charge with end caps, which is based on Huang's formula, was proposed by the theoretical analysis and data fitting and validated experimentally. The results indicate that the proposed formula is accurate in predicting the fragment velocity distribution along the axis of a cylindrical cased charge with end caps detonated at one end.     

A generalized model for estimation of aerodynamic forces and moments for irregularly shaped bodies

A novel method for estimation of an aerodynamic force and moment acting on an irregularly shaped body (such as HE projectile fragments) during its flight through the atmosphere is presented. The model assumes that fragments can be approximated with a tri-axial ellipsoid that has continuous surface given as a mathematical function. The model was validated with CFD data for a tri-axial ellipsoid and verified using CFD data on aerodynamic forces and moments acting on an irregularly shaped fragment.The contribution of this method is that it represents a significant step toward a modeling that does not require a cumbersome CFD simulation results for estimation of fragment dynamic and kinematic parameters. Due to this advantage, the model can predict the fragment motion consuming a negligible time when compared to the corresponding time consumed by CFD simulations. Parametric representation (generalization) of the fragment geometrical data and the conditions provides the way to analyze various correlations and how parameters influence the dynamics of the fragment flight.     

A novel method for determination of lethal radius for high-explosive artillery projectiles

A new model has been defined that enables the estimation of the lethal radius (radius of efficiency) of HE (High Explosive) artillery projectiles against human targets. The model is made of several modules: CAD (Computer Aided Design) modeling, fragment mass distribution estimation, fragment initial velocity prediction, fragment trajectory calculation, effective fragment density estimation, and high explosive projectile lethal radius estimation. The results were compared with the experimental results obtained based on tests in the arena used in our country, and the agreement of the results was good. This model can be used in any terminal-ballistics scenario for high explosive projectiles since it is general, para-metric, fast and relatively easy to implement.     

一种基于SVD的非平稳信号重叠分段降噪算法

在分析基于SVD的平稳信号降噪原理的基础上,提出了一种基于SVD的非平稳信号重叠分段降噪算法.非平稳信号通过数据分段可近似处理为多段平稳信号.为降低连续分段降噪误差,进行一定比例的重叠分段,应用基于SVD的平稳信号降噪方法对各分段信号进行降噪,相邻段之间的重叠信号经过多次降噪后求平均得到最终降噪信号.仿真结果表明,该算...