可变形定向破片战斗部模型试验和数值模拟研究

基于可变形定向破片战斗部的作用原理,设计了试验结构模型,并对其进行了静爆试验研究。根据试验结果,建立了有限元分析模型,利用LS-DYNA程序对可变形定向战斗部变形过程以及破片的飞散过程进行了数值模拟。结果表明,在目标方向破片密度和速度都有较大幅度增益,数值模拟与试验结果比较吻合。     

Interface defeat studies of long-rod projectile impacting on ceramic targets

The interface defeat phenomenon always occurs when a long-rod projectile impacting on the ceramic target with certain velocity, i.e., the projectile is forced to flow radially on the surface of ceramic plates for a period of time without significant penetration. Interface defeat has a direct effect upon the ballistic performance of the armor piercing projectile, which is studied numerically and theoretically at present. Firstly, by modeling the projectiles and ceramic targets with the SPH (Smoothed Particle Hydrodynamics) particles and Lagrange finite elements, the systematic numerical simulations on interface defeat are performed with the commercial finite element program AUTODYN. Three different responses, i.e., complete interface defeat, dwell and direct penetration, are reproduced in different types of ceramic targets (bare, buffered, radially confined and oblique). Furthermore, by adopting the validated numerical algorithms, constitutive models and the corresponding material parameters, the influences of projectile (material, diameter, nose shape), constitutive models of ceramic (JH-1 and JH-2 models), buffer and cover plate (thickness, constraints, material), as well as the prestress acted on the target (radial and hydrostatic) on the interface defeat (transition velocity and dwell time) are systematically investigated. Finally, based on the energy conservation approach and taking the strain rate effect of ceramic material into account, a modified model for predicting the upper limit of transition velocity is proposed and validated. The present work and derived conclusions can provide helpful reference for the design and optimization of both the long-rod projectile and ceramic armor.     

Damage assessment of the target area of the island/reef under the attack of missile warhead

Under the background of vigorously developing facilities of island/reef in the world, the economic value and strategic significance of the island/reef have become increasingly important. Unfortunately, they may easily become the attacking target of missiles in the war time. Therefore, aiming at the damage quantification of the targets in the island/reef under the missile attacking, a macroscopic damage assessment model for the target area is proposed in this paper. The model focuses on the construction of the assessment model framework. Firstly, the analytic hierarchy process and the grey relational analysis are applied to measure the importance of each target in the region through four indicators of the target hazard, striking urgency, damage advantage and mission relevance, respectively. Secondly, based on the damage mechanism of shock wave and fragments to target, the corresponding damage model is established, and the damage grade of each target in the evaluated area is obtained according to the damage criteria and grading standard. Finally, the model obtains the overall damage grade of the target area by employing the fuzzy comprehensive evaluation method, with synthesizing the importance and the damage grade of each target. Through the verification of an example, it demonstrates the certain feasibility of the model and provides a certain basis and reference for the subsequent research.     

装备剩余寿命预测平行仿真中模型动态演化方法

装备平行仿真中的一个重要概念是实时数据驱动的模型动态演化,但是至今仍缺乏具体应用领域的实现方法。以带未知离散冲击的混合退化装备剩余寿命预测为背景,以多态Wiener状态空间模型为演化对象,提出一种装备平行仿真中模型动态演化方法,包括基于交互多模型强跟踪滤波的模型软切换和基于期望最大化算法的模型参数在线估计,并实现了基于平行仿真的装备剩余寿命实时预测。利用某轴承退化数据进行实例研究,结果表明该方法能有效提高仿真逼真度,剩余寿命预测的准确度较高、不确定性较小,具有较高工程应用价值。     

某自行高炮虚拟训练系统设计及关键技术

结合自行式高炮装备的结构特点和训练需求,采用机理与外观相分离的设计思想,建立一种多节点、多任务的分布式仿真训练系统。以机理模型为设计核心,采用了客户/服务器模式的系统拓扑结构。介绍了复杂装备外观建模方法和交互技术以及基于MATLAB的机理模型构建和系统集成方法。     

C~4ISR系统仿真测试研究

针对一种C4ISR系统在测试时的特点,提出了模拟仿真测试的方案,建立了仿真装备与指挥系统的交互模型,设计了交互对象的自动匹配算法,并在实际系统的仿真测试中得到应用和验证。     

一种快速解算火箭助飞鱼雷关机点方法

为解决火箭助飞鱼雷射程与关机点计算速度问题,运用Chebyshev正交多项式拟合曲线,提出了一种基于时间或能量关机的计算方法.可根据不同的射程快速解算助飞雷关机点,达到实时控制助飞雷射程的目的,与现有方法相比,计算简洁、迅速.最后给出了关机方法软件的仿真流程,并将该软件应用于某助飞雷仿真系统,论证了该方法的可行性.     

被动声传感器网络模拟器的设计与实现

现代雷达防空体系对低空/超低空飞行目标的探测仍然是其弱点之一.被动声传感器网络数据融合理论和技术的快速发展,给这类目标的探测、识别和定位跟踪提供了新的方法.在对被动声传感器工作原理、目标运动模型和方位角检测模型分析的基础上,给出了一种被动声传感器网络模拟器的设计思路,同时给出了其软件平台的实现方法.模拟器考虑了大气环境因素的影响和传感器对目标探测的实时处理能力的要求,产生的仿真数据能够较好地逼近真实数据,为被动声传感器数据融合算法的研究提供了强有力的数据支持.     

基于RTX的实时测控系统软件设计

从无人机半物理仿真试验的整体结构出发,针对实时测控系统的需求,采用了一种较为新颖的Windows+RTX实时性方案,完成了无人机半物理仿真试验中实时测控系统的研制.既满足了试验的实时性要求,又具有很好的用户交互特性,对测控技术的发展及其在国防科技等相关领域中的应用均有重要的参考价值.     

一种嵌入式系统中软硬件故障的划分方法

软硬件故障是嵌入式系统可靠性的关键问题之一,如何划分软硬件故障对于整个系统的可靠性研究来说是至关重要的,也是最基本的一步.给出了软硬件故障的基本定义,并与单纯的软件故障和单纯的硬件故障进行了对比,总结了软硬件故障的基本特点.在此基础上,归纳了几条软硬件故障的划分原则,提出了一种软硬件故障的划分流程,并通过形式化方法对某装备的具体软硬件故障进行了划分,为进一步的研究提供了有力的依据.