色噪声环境下MIMO雷达相干目标角度估计算法

针对色噪声环境下的MIMO雷达相干目标角度估计问题,提出一种基于目标信息矢量重构的角度估计算法.算法对MIMO雷达的接收数据进行了低复杂度改进,通过计算四阶累积量,得到一组矢量并证明该矢量包含所有目标的角度信息,通过重构Toeplitz矩阵,结合MUSIC算法实现了色噪声环境下MIMO雷达相干目标的角度估计.算法保留了MIMO雷达的阵元扩展能力和目标分辨力,具有自动抑制加性高斯白噪声和色噪声的能力,实现了相干目标的有效估计,更利于在实际中应用.最后计算机仿真结果证实了算法的有效性和可行性.     

Thermal hazard assessment of TKX-50-based melt-cast explosive

In the present study, thermal hazards of TNT and DNAN used as the molten binder in TKX-50-based melt-cast explosives were comparatively studied through accelerating rate calorimeter (ARC) and Cook-off experiments. Two kinds of ARC operation modes were performed to investigate the thermal safety performance under adiabatic conditions (HWS mode) and constant heating (CHR mode). The obtained results demonstrated that at both heating modes, DNAN/TKX-50 outperformed TNT/TKX-50 from the thermal safety point of view. However, the sensitivity to heat of the samples was reverse because of the different heating modes. In addition, the results of thermal hazard assessment obtained from the cook-off experiment complied with ARC analysis which indicated the molten binder TNT replaced by DNAN would reduce the hazard of the TKX-50 melt cast explosive. Furthermore, the results of cook-off experiments also showed that DNAN/TKX-50 outperformed TNT/TKX-50 from the aspect of thermal stability, which was consistent with the result of CHR mode because of the similar heating process.     

Investigation of the shock compression behaviors of Al/PTFE composites with experimental and a 3D mesoscale-model

The responses of AI/PTFE reactive materials (RMs) under shock compression were investigated by a single-stage gas gun.A 3D mesoscale-model was established based on micro-computed tomography(micro-CT) slice images and confirmed with experimental results.In the high-pressure stage,the com-posites reacted partially,whereas there were no deviations between the partially reacted Hugoniot and the inert simulation results.The simulation reveals that the Teflon matrix melting on the high shock pressure.Melts and decomposition of the PTFE accelerated the diffusion of the atoms.Thus,the reactions of the Al/PrFE composites are more like a combustion rather than a detonation.     

弹道修正弹射程偏差预测与阻力板展开时机优化

根据弹道修正弹阻力板的展开控制对于射程偏差预测要求的实时性,提出基于摄动原理的射程偏差预测算法.为解决阻力板修正能力在线计算数据量大的问题,提出在弹载计算机上装定阻力板修正能力表格的方法,给出发射前计算修正能力表格的过程和飞行中使用修正能力表格的步骤,提出阻力板展开时机的优化判断条件,并采用该方法对某型弹道修正火箭弹射程修正控制进行仿真试验和飞行试验.仿真试验结果表明,当目标射程为33 565.4m时,经修正后火箭弹的射程偏差能控制在20m以内;飞行试验结果表明,弹道修正火箭弹的射程偏差实测为24m,射程精度得到明显提高.     

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。     

C4ISR体系结构设计方法

系统体系结构的设计在C4ISR系统开发中具有重要的地位,文章深入研究了目前运用广泛的三种C4ISR系统体系结构分析设计方法面向过程分析方法、面向对象设计方法和三维视图方法,分析了各种方法的优缺点并进行了比较;讨论了C4ISR体系结构设计方法和C4ISR系统本身的发展趋势以及两者之间的密切关系,对C4ISR系统体系结构的建设提出了自己的看法.     

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。