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101.
《防务技术》2020,16(1):119-135
The behind-armor debris (BAD) formed by the perforation of an EFP is the main damage factor for the secondary destruction to the behind-armor components. Aiming at investigating the BAD caused by EFP, flash X-ray radiography combined with an experimental witness plate test method was used, and the FEM-SPH adaptive conversion algorithm in LS-DYNA software was employed to model the perforation process. The simulation results of the debris cloud shape and number of debris were in good agreement with the flash X-ray radiographs and perforated holes on the witness plate, respectively. Three-dimensional numerical simulations of EFP's penetration under various impact conditions were conducted. The results show that, an ellipsoidal debris cloud, with the major-to-minor axis radio (a/b) smaller than that caused by shaped charge jets, was formed behind the target. With the increase of target thickness (h) and decrease of impact velocity (v0) and obliquity (θ), the value of a/b decreases. The number of debris ejected from target is significantly higher than that from EFP. Based on the statistical analysis of the spatial distribution of the BAD, An engineering calculation model was established considering the influence of h, v0 and θ. The model can with reasonable accuracy predict the quantity and velocity distribution characteristics of BAD formed by EFP. 相似文献
102.
固体灭火剂爆炸抛撒半径分析 总被引:3,自引:0,他引:3
根据爆轰产物等熵膨胀原理和流体动力学理论,通过对灭火剂抛撒3个阶段的理论分析,推导出灭火剂抛撒的理论半径,估算灭火弹的灭火威力。在此基础上进行实爆试验,对两者的值进行比较分析,取得了良好的一致性,为优化灭火弹设计,提高灭火弹威力起着积极的指导作用。 相似文献
103.
基于AHP和云重心方法的装甲兵指挥信息系统效能评估 总被引:2,自引:0,他引:2
针对装甲机械化部队指挥信息系统作战效能评估问题,运用云理论进行了探索。首先,对云重心理论的步骤进行了阐述,结合层次分析法,最后用加权偏离度来衡量系统与理想状态的偏离度,将结果用Matlab三维图形对装甲机械化部队指挥信息系统的作战效能进行描述,图形较直观的反应了其效能问题。此方法简单易行,可操作性强,为装甲机械化部队指挥信息系统评估提供了一种较好的途径。 相似文献
104.
基于云模型的导弹信息作战指挥效能评估 总被引:1,自引:0,他引:1
针对导弹信息作战指挥效能评估中既包含定量指标,又包含定性指标,而对这些指标进行科学合理地统一评价尚存在很多困难的问题,运用云模型对其进行了研究。分析了导弹信息作战指挥能力的指标体系,介绍了云模型的相关理论,并给出了运用云模型进行效能评估的详细算法,利用云发生器得到了最终的评估结果。最后给出了一个评估实例,结果证明该方法有效可行,能很好地解决效能评估中定性语言到定量值之间的转化问题。 相似文献
105.
《防务技术》2020,16(1):69-76
The missile-borne LiDAR has an essential prospect in precise guidance. However, the instability of the missile has a significant impact on the precision of LIDAR point cloud, thus modeling and analyzing the influencing factors of point cloud generation is necessary. In this investigation, the authors modeled the point cloud calculation process of missile-borne linear array scanning LiDAR under ideal conditions and analyzed the effect of position change on the field of view (FOV) in the course of platform motion. Subsequently, the authors summarized that the stability concerning the field of view and the target tracking are dependent on three limiting conditions. Finally, the authors derived an error formula and analyzed several typical errors in missile platform flight, including scanner error, POS error, system integration error, and platform vibration error. Based on theoretical analysis and simulation experiments, the model proposed in this paper can provide a theoretical basis for the design of the missile-borne LiDAR system and the selection of related instruments in practice. 相似文献
106.
由于现代战斗中大量使用各种先进的武器系统和技术装备,我坦克在战场上面临多种不同种类、不同价值、不同威胁程度的射击目标。然而,战场情形瞬息万变,需要考虑的因素错综复杂,因此,需要一种能够应用于指挥控制系统的射击目标选择方法来辅助坦克乘员进行射击目标选择。尝试应用构建云模型的方法对坦克射击目标的特点进行分析,从而得出备选目标的一组排序。 相似文献