基于单片机的远程光纤通信在点对点安全验证系统上的应用

现有的点对点安全验证系统都是基于电缆连接实现系统信息传输的。电缆传输信号存在传输衰减大、抗干扰能力差、在雷暴天气易发生事故等缺点。通过将基于单片机89C2051的远程光纤通信应用到现有设备来改进控制信号的传输模式，将电信号转换为光信号，在数据传输中使用传输同步码加密、数据包CRC校验、串行数据编码以及光纤连通性定时自动监测等技术，可以从物理信号传输到数据接收处理的整个过程中保证系统的安全性和可靠性；同时，通过光纤通信方案，也能节省系统构建和维护的经费。     

基于一类弱连续T-模的模糊Hopfield神经网络研究

基于一般的弱连续T-模与取大（V）模糊算子的复合，建立了具有一般意义的动态模糊神经网络——模糊Hopfield神经网络，并系统分析了该动态系统的性能：在Hamming距离意义下证明了该网络是稳定的，而且其平衡点（吸引子）具有全局Lyapunov稳定性。最后，提供了一种有效的学习算法。     

有限数量机载雷达目标覆盖价值算法

针对有限数量机载雷达目标覆盖价值问题,建立了机载雷达载机待选轨道中心点(COCP)概念;分析了COCP和目标点之间的关系,给出了有限数量机载雷达目标覆盖价值问题的数学模型。通过分析有限规模COCP集合的方法,建立了多个机载雷达部署约束条件的数学模型。通过对COCP集合和目标点集合进行约束排除和聚类,简化了研究问题。总结出了有限数量机载雷达目标覆盖价值数学模型的最优解和启发式次优解,实例仿真结果表明该模型和算法的有效性。     

地球模型偏差对远程弹箭弹道仿真的影响及修正

针对地球模型精确度影响远程弹箭弹道仿真的问题,分析了地球模型偏差对弹道仿真精度的影响并加以修正。采用总的地球椭球系,在已有弹道模型的基础上,分析了垂线偏差的产生机理及其对定向定位参数的影响,并由此得出弹道几何偏移随定向偏差的变化规律,研究了引力加速度初值偏差对弹道的误差累积,并对由水准面不平行性造成的实际落点高差进行了理论推导。对比仿真算例表明,考虑地球模型偏差影响的仿真结果与不考虑的情况下差别较明显,在远程条件下对弹道仿真精度的影响不容忽视。     

飞航导弹故障飞行落点概率计算方法

针对飞航导弹故障飞行落点概率难以准确计算的问题,通过分析导弹的各个分系统的故障机理重新提出五种故障模式,依据逐系统串联的原理建立了故障模式的概率分配计算模型;在对发射、飞行和故障后坠落等阶段进行分析的基础上建立各故障模式的仿真模型;最后应用蒙特卡洛方法对某型导弹故障飞行落点的概率分布进行了仿真计算。     

旋转永磁式机械低频天线的系统设计与验证

为实现低频电磁发信系统的小型化和低功耗,面向旋转永磁式机械天线的理论研究和技术实践,提出了基于多物理场耦合仿真的系统设计和性能校验方法。设计了包含永磁磁源、高效驱动电机及其控制器在内的旋转永磁式机械天线系统方案。研制了实验样机,并对其系统性能和近区磁场进行了实验测试,验证了相关设计方法和系统方案的可行性与有效性。结果表明,该样机的磁场场强和尺寸等主要指标达到了美国“机械天线”项目在射频穿透技术领域的要求,为旋转永磁式机械天线方案研究和样机设计提供了一种可行思路。     

Sensor placement in active multistatic sonar networks

The idea of deploying noncollocated sources and receivers in multistatic sonar networks (MSNs) has emerged as a promising area of opportunity in sonar systems. This article is one of the first to address point coverage problems in MSNs, where a number of points of interest have to be monitored in order to protect them from hostile underwater assets. We consider discrete “definite range” sensors as well as various diffuse sensor models. We make several new contributions. By showing that the convex hull spanned by the targets is guaranteed to contain optimal sensor positions, we are able to limit the solution space. Under a definite range sensor model, we are able to exclude even more suboptimal solutions. We then formulate a nonlinear program and an integer nonlinear program to express the sensor placement problem. To address the nonconvex single‐source placement problem, we develop the Divide Best Sector (DiBS) algorithm, which quickly provides an optimal source position assuming fixed receivers. Starting with a basic implementation of DiBS, we show how incorporating advanced sector splitting methods and termination conditions further improve the algorithm. We also discuss two ways to use DiBS to find multiple source positions by placing sensors iteratively or simultaneously. © 2017 Wiley Periodicals, Inc. Naval Research Logistics 64: 287–304, 2017     

融合空间偏好和语义的个体活动识别方法

个体活动识别对用户画像、个性化推荐、异常行为检测、群体行为分析和基于活动的资源配置优化具有重要价值。提出了一种基于稀疏的社交媒体签到数据的个体活动语义识别方法,从签到数据中提取活动行为的时间周期性和趋势性特征,并采用空间偏好量化算法,从个体与群体活动的空间关联中提取群体和个体的空间访问偏好,使用自然语言嵌入工具BERT模型提取访问兴趣点的语义。时间特征、空间偏好特征和访问兴趣点名称语义特征共同构成表征群体、个体偏好的时空联合特征,通过极限梯度提升分类器对其进行分类,得到活动语义识别结果。在Foursquare数据集上的对比实验和消融实验中验证了所提活动语义识别模型可以有效提升活动语义识别的准确性。     

A study on the surface overpressure distribution and formation of a double curvature liner under a two-point initiation

The formation mechanism of an EFP(explosively formed projectile) using a double curvature liner under the overpressure effect generated by a regular oblique reflection was investigated in this paper.Based on the detonation wave propagation theory,the change of the incident angle of the detonation wave collision at different positions and the distribution area of the overpressure on the surface of the liner were calculated.Three-dimensional numerical simulations of the formation process of the EFP with tail as well as the ability to penetrate 45# steel were performed using LS-DYNA software,and the EFP ve-locity,the penetration ability,and the forming were assessed via experiments and x-ray photographs.The experimental results coincides with those of the simulations.Results indicate that the collision of the detonation wave was controlled to be a regular oblique reflection acting on the liner by setting the di-mensions of the unit charge and maintaining the pressure at the collision point region at more than 2.4 times the CJ detonation when the incident angle approached the critical angle.The distance from the liner midline to the boundary of the area within which the pressure ratio of the regular oblique reflection pressure to the CJ detonation pressure was greater than 2.5,2,and 1.5was approximately 0.66 mm,1.32 mm,and 3.3 mm,respectively.It is noted that pressure gradient caused the liner to turn inside out in the middle to form the head of the EFP and close the two tails of the EFP at approximately 120μs.The penetration depth of the EFP into a 45# steel target exceeded 30 mm,and there was radial expansion between the head and tail of the EFE increasing the penetration resistance of the EFP.Therefore,the structural size of the unit charge and the liner can be further optimized to reduce resistance to increase the penetration ability of the EFP.     

基于随机拟合的悬浮式深弹弹阵特征建模

通过分析悬浮式深弹发射后在空中的弹道特性,建立了深弹弹着点坐标的计算模型。采取蒙特卡洛方法,分别对舰艇六自由度状态下,单管和六联装火箭深弹的弹着点坐标进行了仿真计算,对弹着点的分布规律进行了研究,并得出弹着点的联合密度函数。结果表明,在发射参数存在正态扰动下,弹着点散布区域均呈椭圆形分布,弹着点坐标均仍服从正态分布。