基于加权的目标综合识别技术

在基于证据理论的目标综合识别系统中,综合考虑信息源权重对识别结果有重要的影响.提出了基于加权的目标综合识别技术,总结了几种常用的主观权重和客观权重获取方法,给出了组合权重的计算公式,针对D-S证据理论仿真验证了基于证据加权思想对合成结果的改进效果.研究表明,在进行目标综合识别时考虑信息源的权重是必要的,它能有效化解信源冲突,保证合成结果的合理性和稳健性.     

双通道短时互谱法的潜艇目标尺度识别

阐述了双通道短时互谱法的基本理论,分析了目标方位走向,提出了利用体目标回波的空间方位分布信息识别水下目标尺度的方法。最后采用潜艇目标亮点模型,通过计算机仿真给出了目标方位走向拟合示意图,给出了在不同攻击阵位的条件下,鱼雷对潜艇目标进行尺度识别的估计值和估计方差并进行了相应的分析,确定了最有利于目标识别的攻击弦角。     

基于熵的空中目标识别模型及应用

空中目标识别是现代防空作战的重要研究内容。研究根据不同类型的目标产生不同的辐射和不同的雷达回波信号对目标进行识别。提出利用熵理论来处理目标识别问题,采用层次分析法与熵权的组合来确定指标的权重。仿真实例表明,基于熵的识别是一种运算简单,结果可靠的目标识别算法。     

时域分析在雷达动目标识别中的应用

本文通过对地面几类目标运动特性的统计研究,利用线性预测的方法进行目标特征的提取,进而用模式识别的理论对地面目标进行自动识别,取得了良好的识别效果。     

求吊声一次搜潜概率的新方法

本文用不同于既往的研究方法,从对目标运动要素散布的分析入手,较合理地假设了目标的运动,进而用数学分析方法推得吊放声纳一次搜潜概率的解析模型。这一模型的突出特点是计算简便、实用性强,各参数的含义一目了然。     

瞄准具多因素误差分析模型

本文利用坐标轴旋转公式建立了瞄准具多因素误差分析模型。为机械式、半独立式瞄准具的不解体检测提供了理论基础.     

型号研制技术状态管理

论述了型号工程研制项目的技术状态管理目标、技术状态管理的４个基本功能（即标识、控制、状态记实与审核）的管理过程,及３个技术状态基线建立的时机。     

球头弹低速斜侵彻下薄板穿甲破坏机理研究

为探讨球头弹低速斜侵彻下靶板的破坏机理,通过系列弹道试验,对比分析了不同初始速度下弹体的变形,靶板的破坏模式,以及靶板的破口大小及形状;同时采用ANSYS/LS-DYNA对弹靶作用过程进行了数值模拟。结果表明：低速斜侵彻下靶板响应非完全对称,根据受力特征可将靶板划分为四个不同区域,即接触区,弯曲区,拉伸区和对称区;薄板的穿甲破坏可分为四个不同的阶段,即隆起变形,碟形变形,弯曲变形,弹体贯穿阶段;不同初始速度下靶板出现四种典型的穿甲破坏模式,随着初始速度的增加依次为隆起—碟形变形,隆起—碟形变形—拉弯撕裂破坏,隆起—碟形变形—拉弯剪切破坏,隆起—拉弯剪切破坏。斜侵彻下靶板破口形状为椭圆形,随着初始速度的增加,破口长径不断减小,形状由椭圆形向卵形过渡。     

Path planning for moving target tracking by fixed-wing UAV

For the automatic tracking of unknown moving targets on the ground, most of the commonly used methods involve circling above the target. With such a tracking mode, there is a moving laser spot on the target, which will bring trouble for cooperative manned helicopters. In this paper, we propose a new way of tracking, where an unmanned aerial vehicle (UAV) circles on one side of the tracked target. A circular path algorithm is developed for monitoring the relative position between the UAV and the target considering the real-time range and the bearing angle. This can determine the center of the new circular path if the predicted range between the UAV and the target does not meet the monitoring requirements. A transition path algorithm is presented for planning the transition path between circular paths that constrain the turning radius of the UAV. The transition path algorithm can generate waypoints that meet the flight ability. In this paper, we analyze the entire method and detail the scope of applications. We formulate an observation angle as an evaluation index. A series of simulations and evaluation index comparisons verify the effectiveness of the proposed algorithms.     

Attitude deflection of oblique perforation of concrete targets by a rigid projectile

A perforation model is developed to predict the attitude deflection in the oblique perforation of concrete targets by a rigid projectile, in which the inertial moment of the projectile is introduced, together with taking the attitude deflection during the shear plugging sub-stage into account, and the shape of the plug formed on the rear surface of target is also re-investigated. Moreover, a new classification of concrete targets is proposed based on the target thickness, with which the attitude deflections in different kinds of concrete targets are analyzed. It is found that the numerical results by using the new perforation model are in good agreement with the previous experimental data and simulated results. Furthermore, the variations of the attitude deflection with the initial conditions (the initial attitude angle and the initial impact velocity) are investigated.