基于黑板模型的空袭目标识别专家系统

在对空袭目标信息进行综合利用的基础上,建立了基于黑板模型的多传感器空袭目标识别融合专家系统模型,模拟专家识别思维.给出了知识库的构造方法和知识的表示方法;推理机的设计结合了问题求解的黑板模型和D-S证据推理方法.该模型对目标的综合应用识别具有很好的借鉴作用,测试表明该系统具有很强的推理能力,融合模型有较高的识别准确性和可靠性.     

一种基于加权DSmT的序列图像目标识别方法

通过对自动目标识别系统研究与分析,将DSmT引入到飞机序列图像识别中,构建基本置信指派及分类规则,提出了一种基于加权DSmT的序列图像目标识别方法,在分析权值选择特点的基础上,根据特征信息的置信指派组合有效权值,并且给出了基于加权DSmT融合规则的序列图像目标识别的流程,仿真结果表明,该方法提高了序列图像目标识别的准确性.     

动态武器目标分配问题的马尔可夫性

动态武器目标分配(weapon target assignment,WTA)问题是军事运筹学研究的重要理论问题,也是作战指挥决策中迫切需要解决的现实问题。在对动态WTA问题进行描述分析的基础上,运用随机过程理论证明了动态WTA过程的马尔可夫性;给出了该马尔可夫决策过程的状态转移概率的解析表达式,并对其状态特点进行了简要分析。研究结果可以为动态WTA及相关问题的研究提供理论和方法依据。     

一种单像机对运动目标定位的新方法

运动目标的空间位置确定是光学测量的重要内容,具有十分广泛的工程应用背景。针对无目标距离信息和目标上已知控制点的单像机成像情况,通过假设目标服从某种运动规律,增加目标定位的约束信息,提出了一种单像机对运动目标定位的新方法:共线方程法。仿真计算证明了此方法的正确性和可行性。     

不确定环境下无人机区域目标搜索及载荷参数影响

针对不确定环境下无人机区域搜索问题,建立了实时探测更新的搜索方法,提出了机载光电载荷参数优化配置策略。建立了基于二维离散网格的无人机区域搜索模型,采用概率地图描述目标信息的实时获取与更新;引入不确定度指标、目标网格的重访和网格探测次数控制,建立搜索目标函数;建立了基于粒子群算法的搜索路径滚动优化方法;通过对任务区域平均探测时间步数和误判概率的估计分析,建立了机载光电载荷参数优化配置策略。使用蒙特卡洛方法验证了区域搜索方法的有效性和光电载荷参数配置对搜索效率、误判概率的影响。     

Shaped charge penetration into high- and ultrahigh-strength Steel–Fiber reactive powder concrete targets

Experiments on shaped charge penetration into high and ultrahigh strength steel-fiber reactive powder concrete (RPC) targets were performed in this paper. Results show that the variation of penetration depth and crater diameter with concrete strength is different from that of shaped charge penetration into normal strength concrete (NSC). The crater diameter of RPC is smaller than that of NSC penetrated by the shaped charge. The jet particles are strongly disturbed and hardly reach the crater bottom because they pass through the narrow channel formed by jet penetration into the RPC. The effects of radial drift velocity and gap effects of jet particles for a shaped charge penetration into RPC target are discussed. Moreover, a theoretical model is presented to describe the penetration of shaped charge into RPC target. As the concrete strength increases, the penetration resistance increases and the entrance crater diameter decreases. Given the drift velocity and narrow crater channel, the low-velocity jet particles can hardly reach the crater bottom to increase the penetration depth. Moreover, the narrow channel has a stronger interference to the jet particles with increasing concrete strength; hence, the gap effects must be considered. The drift velocity and gap effects, which are the same as penetration resistance, also have significant effects during the process of shaped charge penetration into ultrahigh-strength concrete. The crater profiles are calculated through a theoretical model, and the results are in good agreement with the experiments.     

A novel facial emotion recognition scheme based on graph mining

Recent years have seen an explosion in graph data from a variety of scientific, social and technological fields. From these fields, emotion recognition is an interesting research area because it finds many applications in real life such as in effective social robotics to increase the interactivity of the robot with human, driver safety during driving, pain monitoring during surgery etc. A novel facial emotion recognition based on graph mining has been proposed in this paper to make a paradigm shift in the way of representing the face region, where the face region is represented as a graph of nodes and edges and the gSpan frequent sub-graphs mining algorithm is used to find the frequent sub-structures in the graph database of each emotion. To reduce the number of generated sub-graphs, overlap ratio metric is utilized for this purpose. After encoding the final selected sub-graphs, binary classification is then applied to classify the emotion of the queried input facial image using six levels of classification. Binary cat swarm intelligence is applied within each level of classification to select proper sub-graphs that give the highest accuracy in that level. Different experiments have been conducted using Surrey Audio-Visual Expressed Emotion (SAVEE) database and the final system accuracy was 90.00%. The results show significant accuracy improvements (about 2%) by the proposed system in comparison to current published works in SAVEE database.     

高超声速滑翔导弹气动参数自适应跟踪建模

针对高超声速滑翔导弹跟踪中状态模型构建问题,研究基于制导变量变化规律的气动参数建模方法。对气动参数进行分析,指出传统建模方法的缺点。在假设制导变量服从一阶时滞过程的前提下,利用线性化的气动系数推导气动参数模型,通过分析不同飞行状态下的模型变式,证明模型对目标机动具有自适应性。对模型中未知参数的取值问题进行讨论,实现模型与飞行状态的自适应匹配。仿真结果表明：当目标发生机动时,所提模型性能明显优于传统模型。同时,在不同滤波器参数条件下的仿真结果进一步证实了模型的有效性。     

针对不同视场辅助信标的无人机目标定位方法

针对无人机在单站测角测距的目标定位过程中受无人机姿态角误差影响较大的问题,提出一种对辅助信标进行探测并与惯性传感器相结合的无人机姿态求解方法。建立基于容积卡尔曼滤波的惯性传感器姿态求解模型,采用梯度下降法对基于辅助信标的无人机位姿参数进行求解,并综合它们的结果对无人机的姿态偏差进行估计和校正,最后完成了不同视场条件下的目标定位和仿真计算。结果表明,所提方法对无人机目标定位精度有明显提高。     

船舶降噪工程技术集成优化方法

在用船舶降噪工程受总体约束强、声学异常多等因素影响,传统新船建造的声学设计方法不能被直接应用。为此,提出了在用船舶降噪工程技术集成优化方法。根据需求设计顶层降噪指标,并通过四项标准进行检验;基于改装前测试数据和降噪技术储备情况,制定初步降噪技术集成方案;通过声学评估迭代,形成优化的指标分配体系和最终的降噪技术集成方案。模型试验验证结果表明,该方法能够有效实现在用船舶降噪工程的技术优化集成。