装备保障综合演练风险分析

采用工作结构分解(Work Breakdown Structure,WBS)和风险结构分解法(Risk Breakdown Structure,RBS)对装备保障综合演练全过程的风险及其风险因素进行了系统分析,得出了装备保障综合演练过程中存在的7类风险、24种风险因素;运用网络层次分析法(Analytic Network Process,ANP)对各种风险及其风险因素进行了评估,得出了其对装备保障综合演练风险影响的权重及排序。研究结果可为装备保障综合演练顺利开展,确保人员、装备安全提供参考。     

Deconsolidation and combustion performance of thermally consolidated propellants deterred by multi-layers coating

Both heating and solvent-spray methods are used to consolidate the standard grains of double-base oblate sphere propellants plasticized with triethyleneglycol dinitrate (TEGDN) (TEGDN propellants) to high density propellants. The obtained consolidated propellants are deterred and coated with the slow burning multi-layer coating. The maximum compaction density of deterred and coated consolidated propellants can reach up to 1.39 g/cm³. Their mechanic, deconsolidation and combustion performances are tested by the materials test machine, interrupted burning set-up and closed vessel, respectively. The static compression strength of consolidated propellants deterred by multi-layer coating increases significantly to 18 MPa, indicating that they can be applied in most circumstances of charge service. And the samples are easy to deconsolidate in the interrupted burning test. Furthermore, the closed bomb burning curves of the samples indicate a two-stage combustion phenomenon under the condition of certain thickness of coated multi-layers. After the outer deterred multi-layer coating of consolidated samples is finished burning, the inner consolidated propellants continue to burn and breakup into aggregates and grains. The high burning progressivity can be carefully obtained by the smart control of deconsolidation process and duration of consolidated propellants. The preliminary results of consolidated propellants show that a rapid deconsolidation process at higher deconsolidation pressure is presented in the dynamic vivacity curves of closed bomb test. Higher density and higher macro progressivity of consolidated propellants can be obtained by the techniques in this paper.     

雷达虚拟维修训练中交互系统的通用性

基于USB接口技术对"通用雷达装备虚拟维修训练系统(URVMTS)"的人机交互系统进行研究,通过合理的软、硬件设计实现了系统的通用性。不同的实装操作部件经过适当的信号调理均可以通过该系统方便地实现与雷达虚拟样机之间的交互。着重介绍了交互系统的通用性设计与实现方法,包括系统的通用性设计方案,USB硬件电路的通用性设计及相应的软件开发。     

DIS的多武器模拟器训练系统

现有的武器系统模拟器大多是对单个武器系统平台的性能仿真,利用DIS可以将它们联结成多武器平台的作战环境下的对抗仿真。在分析基于DIS的多武器系统模拟器训练系统的基础上,确定了系统的仿真框架,介绍了系统中通信的实现方法,并介绍了系统的工作过程。     

广义模型的音频分析方法

目前网络数据中包含有大量的多媒体数据,音频作为多媒体信息的重要载体之一,蕴涵了丰富的语义,有效地丰富和补充了人们对信息的感知和获取。而目前的多媒体检索主要利用的是常规的信息检索技术诸如视觉信息,往往忽略了音频信息,这已不能满足需要。音频信息检索就逐渐成为多媒体信息检索的研究重点之一。基于此,针对音频信息检索问题展开讨论,提出一种利用广义模型进行音频分析的新方法。该方法可应用到音频检索中,实验证明了该方法的有效性。     

无源单站定位技术研究

无源定位技术已成为现代化战争中对抗"四大威胁"的关键技术。在研究目标来波方向(DOA)与多普勒频率的基础上,提出一种基于最小二乘估计的运动目标单站定位跟踪方法。经计算机仿真表明,该方法不仅能对运动目标进行定位,而且能对运动目标的速度、航迹等进行估计。     

一种基于LVQ的语音线谱对参数量化方法

在现有格型矢量量化(LVQ)方法的基础上,通过对线谱对(LSP)参数进行精度预处理,使其数值更接近于格点从而减少量化失真。仿真实现了改进方法,并采用MELP算法中4级MSVQ方法作为对比。得到的结果表明,较之MSVQ,LVQ量化LSP参数的精度提升了约90%的同时,合成语音的谱失真(SD)降低了约2/3,客观评估得分和近似MOS分略有提高。     

A general model of heterogeneous system lifetimes and conditions for system burn‐in

Burn‐in is a technique to enhance reliability by eliminating weak items from a population of items having heterogeneous lifetimes. System burn‐in can improve system reliability, but the conditions for system burn‐in to be performed after component burn‐in remain a little understood mathematical challenge. To derive such conditions, we first introduce a general model of heterogeneous system lifetimes, in which the component burn‐in information and assembly problems are related to the prediction of system burn‐in. Many existing system burn‐in models become special cases and two important results are identified. First, heterogeneous system lifetimes can be understood naturally as a consequence of heterogeneous component lifetimes and heterogeneous assembly quality. Second, system burn‐in is effective if assembly quality variation in the components and connections which are arranged in series is greater than a threshold, where the threshold depends on the system structure and component failure rates. © 2003 Wiley Periodicals, Inc. Naval Research Logistics 50: 364–380, 2003.     

潜射弹道导弹出水姿态分析

分析了潜艇深度、纵倾角、横倾角、海面风速、海面波长、平均波高等因素对潜射导弹的偏航角、俯仰角、滚动角、偏航角速度、俯仰角速度、滚动角速度的影响。由于实验数据比较分散,不适合神经网络的训练,所以首先对实验数据模糊化,并用以对神经网络的训练。用训练好的神经网络分析了潜艇单因素变化的导弹出水姿态。     

武器装备排气系统红外抑制器技术综述

主要介绍了排气系统红外抑制器的原理,归纳了建立抑制器模型的方法,列举了多种提高红外抑制器性能的方案和一些重要实验结果。同时对抑制器发展现状进行了介绍和总结,并作出了比较和展望。