12.7mm高射机枪模态试验与分析

本文利用实验模态分析技术和有限元法研究机枪—土壤系统的动态特性,通过模态试验获得机枪在硬质土壤支撑条件下的低阶模态信息,据此对机枪有限元模型的边界条件进行模拟,并从动力学角度分析影响射击精度的主要因素,为进一步研究机枪结构动力修改和质量评估提供依据,     

空气采样早期探测系统应用前景展望

介绍了空气采样早期探测系统的原理,通过将其与常见的常规探测器相比较,充分探讨了不同探测环境下的优越性所在。其中,着重分析了其极早期报警、准确探测火灾、不产生误报的特点。通过对空气采样早期探测系统在国外发展历史的分析,并结合我国的实际情况,认为这种探测方式将在我国得到广泛应用,并会根据我国的国情不断继续发展完善。     

带三维落角约束的寻的导弹制导与姿控系统设计

针对带三维落角约束的寻的导弹制导与姿态控制系统设计问题,提出一种基于终端滑模控制和扩张状态观测器的六自由度制导控制系统设计方法。建立包含模型不确定项的寻的导弹六自由度质心与绕质心模型,设计内外双层环路六自由度制导控制系统框架;基于弹-目三维相对运动模型和坐标系转移矩阵建立以攻角和侧滑角为输入的三维全耦合导引方程,利用终端滑模控制方法和扩展状态观测器得到期望的攻角和侧滑角并将其转化为对应的俯仰、偏航和滚转角指令;根据线性形式的寻的导弹绕质心动力学方程,设计与俯仰、偏航和滚转角相关的滑模面向量,并利用终端滑模控制方法和扩张状态观测器得到寻的导弹的副翼偏角、方向舵偏角和俯仰舵偏角指令。六自由度数值仿真结果验证了该方法的有效性和鲁棒性,并证明了该制导控制系统设计方法能以较少的控制设计参数完成预设的制导控制任务。     

基于规则的CGF实体行为建模技术

CGF行为建模的目的是使行为模型能更好地体现出人类行为特征,提高作战仿真系统的可信性和科学性。在介绍CGF、CGF行为建模概念的基础上,对当前几种主要的CGF行为建模方法进行了比较,并分析了CGF行为模型的一般结构。构建了基于规则的CGF行为模型,重点对基于规则CGF行为模型的决策推理方法进行了研究。采用产生式规则方法对决策知识进行了描述,定义了决策推理过程中的3个要素:态势、动作、决策推理,并对其决策推理过程进行了研究。     

初中生情绪不安全感与攻击行为的关系

本文基于情绪安全感理论,探讨初中生情绪不安全感与攻击行为的关系,采用问卷调查的方式,对新疆某市区274名初中生进行调查。结果显示:①初三年级间接攻击水平显著高于初一年级(F=4.41,p<0.05);②初一、初二年级情绪不安全感水平显著高于初三年级(F=8.31,p<0.001);③初中生情绪不安全感与攻击行为之间存在显著正相关(r=0.32,p<0.01)。调查结果表明,降低初中生的情绪不安全感水平,有助于减少其攻击行为的发生。     

舰船结构塑性动力响应研究进展

从舰船结构塑性动力响应的工程背景出发,简要介绍了该问题当前的研究进展．主要评述了国内外学者所关注的一些基本问题和研究方法,主要包括解析法、近似法、数值法等,以及冲击载荷作用下梁、板、板架、壳体等结构塑性动力响应的研究进展．     

基于用户相关反馈的排序学习算法研究

在信息检索中,系统需要根据用户查询将文档按照相似度大小进行排序,吸引了众多信息检索和机器学习领域研究者的眼球,并形成了诸多排序算法模型。然而并未考虑到查询短语与文档构成的特征对与用户相关反馈之间存在的同质性。在机器学习算法基础上,通过提取训练样本的主要特征进行有效聚类,并结合用户的相关反馈获取各个类中相关度判断的置信值,形成相似度判定模型,应用该模型来对测试样本进行相关度排序。算法对LETOR数据集进行了测试,实验表明,信息检索性能指标比其他排序算法有了进一步提高,并且无需复杂的数据预处理工作和手动设定算法参数。     

背景音乐对人类学习效率影响的脑与行为研究进展

背景青乐是与主体的意识或行为无直接关系,通过非青乐鉴赏环境这一媒介间接作用于主体意识与行为的音乐。近些年来将背景音乐引入教育领域来探讨其对学习效率的影响是研究的新课题。从背景音乐对学习效率影响的相关理论、背景音乐对学习效率影响的实验研究以及背景音乐影响的研究趋势等方面进行了综述。     

Multi-objectives nonlinear structure optimization for actuator in trajectory correction fuze subject to high impact loadings

This paper presents an actuator used for the trajectory correction fuze, which is subject to high impact loadings during launch. A simulation method is carried out to obtain the peak-peak stress value of each component, from which the ball bearings are possible failures according to the results. Subsequently, three schemes against impact loadings, full-element deep groove ball bearing and integrated raceway, needle roller thrust bearing assembly, and gaskets are utilized for redesigning the actuator to effectively reduce the bearings' stress. However, multi-objectives optimization still needs to be conducted for the gaskets to decrease the stress value further to the yield stress. Four gasket's structure parameters and three bearings' peak-peak stress are served as the four optimization variables and three objectives, respectively. Optimized Latin hypercube design is used for generating sample points, and Kriging model selected according to estimation result can establish the relationship between the variables and objec-tives, representing the simulation which is time-consuming. Accordingly, two optimization algorithms work out the Pareto solutions, from which the best solutions are selected, and verified by the simulation to determine the gaskets optimized structure parameters. It can be concluded that the simulation and optimization method based on these components is effective and efficient.     

Damage modeling of ballistic penetration and impact behavior of concrete panel under low and high velocities

This work presents a numerical simulation of ballistic penetration and high velocity impact behavior of plain and reinforced concrete panels. This paper is divided into two parts. The first part consists of numerical modeling of reinforced concrete panel penetrated with a spherical projectile using concrete damage plasticity (CDP) model, while the second part focuses on the comparison of CDP model and Johnson-Holmquist-2 (JH-2) damage model and their ability to describe the behavior of concrete panel under impact loads. The first and second concrete panels have dimensions of 1500 mm × 1500 mm × 150 mm and 675 mm × 675 mm × 200 mm, respectively, and are meshed using 8-node hexahedron solid elements. The impact object used in the first part is a spherical projectile of 150 mm diameter, while in the second part steel projectile of a length of 152 mm is modeled as rigid element. Failure and scabbing characteristics are studied in the first part. In the second part, the com-parison results are presented as damage contours, kinetic energy of projectile and internal energy of the concrete. The results revealed a severe fracture of the panel and high kinetic energy of the projectile using CDP model comparing to the JH-2 model. In addition, the internal energy of concrete using CDP model was found to be less comparing to the JH-2 model.