基于PCI总线的搜索雷达视频模拟器设计技术

针对目前在军用信息技术领域对搜索雷达视频模拟器大目标批数和高实时性的需求,运用PCI总线和FPGA技术设计搜索雷达视频模拟器系统。在设计方面提出了4个硬件设计要点和1个软件设计结构框图,形成了一个完整的搜索雷达视频模拟器系统解决方案。该方案有效地提高了搜索雷达视频模拟器系统的性能,在军用信息技术领域有较广阔的应用。     

激光照射指示器束散角数字化检测方法研究

激光末端制导武器系统中,激光照射指示器出射激光的束散角是一个重要的参数。介绍了一种出射激光束散角的数字化检测方法。区别于传统的套孔法和反射靶板法,该方法通过CCD采集激光光斑,用质心法确定光斑中心,根据激光能量密度分布确定激光光斑半径,进而计算出待测的激光束散角。     

基于自相关的匀速运动模糊尺度参数识别

运动模糊图像复原主要取决于点扩散函数(PSF)的确定。对于匀速直线和匀速旋转运动模糊图像,运动方向和模糊尺度决定了PSF,是重要参数。根据模糊图像的像素点具有高度相关的特性,采用差分和自相关等技术,精确确定模糊尺度,为图像复原提供必要参数。仿真实验验证了该方法的正确性和有效性。     

某型飞机魔球信号采集与分析

从阐述魔球操作对目标瞄准的实现机制入手,分析了数据采集系统的总体结构及采集系统的硬件设计和软件设计思想.实现了对飞机魔球信号的实时采集,并对采集结果进行仿真分析,从而推导出不同相关武器种类、目标与弹轴不同夹角、不同目标距离、不同工作状态下魔球信号的变化规律.     

浅析构建一体化装备保障体系的途径

以一体化联合作战为背景,立足现实装备保障体系基础,着眼未来装备保障体系发展,从一体化装备保障体系的概念、基本特征入手,在树立一体化保障观念、建立装备指挥信息系统、编配合成多能的保障力量、构建军地一体的装备保障模式、培养高素质的装备人才队伍等方面,分析了构建一体化装备保障体系的途径。     

Research on the influences of confining pressure and strain rate on NEPE propellant: Experimental assessment and constitutive model

In order to study the influences of confining pressure and strain rate on the mechanical properties of the Nitrate Ester Plasticized Polyether (NEPE) propellant, uniaxial tensile tests were conducted using the self-made confining pressure system and material testing machine. The stress-strain responses of the NEPE propellant under different confining pressure conditions and strain rates were obtained and analyzed. The results show that confining pressure and strain rate have a remarkably influence on the mechanical responses of the NEPE propellant. As confining pressure increases (from 0 to 5.4 MPa), the maximum tensile stress and ultimate strain increase gradually. With the coupled effects of confining pressure and strain rate, the value of the maximum tensile stress and ultimate strain at 5.4 MPa and 0.0667 s⁻¹ is 2.03 times and 2.19 times of their values under 0 MPa and 0.00333 s⁻¹, respectively. Afterwards, the influence mechanism of confining pressure on the NEPE propellant was analyzed. Finally, based on the viscoelastic theory and continuous damage theory, a nonlinear constitutive model considering confining pressure and strain rate was developed. The damage was considered to be rate-dependent and pressure-dependent. The constitutive model was validated by comparing experimental data with predictions of the constitutive model. The whole maximum stress errors of the model predictions are lower than 4% and the corresponding strain errors are lower than 7%. The results show that confining pressure can suppress the damage initiation and evolution of the NEPE propellant and the nonlinear constitutive model can describe the mechanical responses of the NEPE propellant under various confining pressure conditions and strain rates. This research can lay a theoretical foundation for analyzing the structural integrity of propellant grain accurately under working pressure loading.     

An experiment evaluating how the tiny mass eccentricities in spin-stabilized projectiles affect the position of impact points

This study investigates and quantifies some possible sources affecting the position of impact points of small caliber spin-stabilized projectiles (such as 12.7 mm bullets). A comparative experiment utilizing the control variable method was designed to figure out the influence of tiny eccentric centroids on the projectiles. The study critically analyzes data obtained from characteristic parameter measurements and precision trials. It also combines Sobol's algorithm with an artificial intelligence algorithm—Adaptive Neuro-Fuzzy Inference Systems (ANFIS)—in order to conduct global sensitivity analysis and determine which parameters were most influential. The results indicate that the impact points of projectiles with an entry angle of 0° deflected to the left to that of projectiles with an entry angle of 90°. The difference of the mean coordinates of impact points was about 12.61 cm at a target range of 200 m. Variance analysis indicated that the entry angle — i.e. the initial position of mass eccentricity — had a notable influence. After global sensitivity analysis, the significance of the effect of mass eccentricity was confirmed again and the most influential factors were determined to be the axial moment and transverse moment of inertia (Izz Iyy), the mass of a projectile (m), the distance between nose and center of mass along the symmetry axis for a projectile (Lm), and the eccentric distance of the centroid (Lr). The results imply that the control scheme by means of modifying mass center (moving mass or mass eccentricity) is promising for designing small-caliber spin-stabilized projectiles.     

小型地面机器人链路通信距离测试方法设计

针对复杂环境条件下小型地面机器人链路通信距离测试方法问题,分析并指出了传统链路通信距离测试方法无法适用于地面机器人测试的原因,根据小型地面机器人使用环境和无线链路近地传播特点,选取对数距离路径损耗模型改进了传统测试方法,并在3种典型环境下进行了实地测试验证,结果表明:新方法能通过定量数据揭示被测机器人在不同环境下链路通信环境的差异性,适用于复杂环境下小型地面机器人链路通信距离测试.     

电磁炮炮管振动信号分析及处理方法

炮管发射振动是影响电磁炮发射稳定性及射击精度的关键因素,获取炮管振动信号有效数据,对优化其发射性能具有重要的意义.在对电磁炮炮管振动信号分析的基础上,提出了采用小波阈值去噪和最小二乘法相结合的信号处理方法来去除振动干扰信号,通过仿真实验,理论验证了该信号处理方法的有效性;设计测试系统进行振动实测实验,并使用该信号处理方法获得振动有效信号,进一步验证了该方法的有效性和实用性;计算得到炮管振动位移参量,为电磁炮设计、优化提供了理论依据.     

国防科技工业专利研究

本文主要阐述了国防专利的基本特点,分析了我国国防专利的现状、问题及制约因素,针对我国实施知识产权战略的要求,结合国防专利的特点,研究提出了加强国防专利保护的若干对策。