单装战损评估仿真系统的设计与实现

首先介绍了系统模型的建立;接着阐述了系统功能、结构以及各子系统的设计与实现;继而介绍了系统实现所用到的关键技术和方法;最后利用该系统,进行了某杀爆战斗部对卡车毁伤的仿真试验,得出了汽车部件毁伤分布及毁伤等级等结果。仿真结果表明,该仿真结果与试验数据基本吻合。该系统可以为维修保障及器材供应计划的制定提供参考依据。     

基于改进遗传算法的结构损伤识别

结构损伤识别问题在数学上可以转化为一种带约束的目标函数优化求解。将基于混沌系统的优化理论和免疫系统的基本机制提出的自适应免疫遗传算法用于结构损伤识别,研究其有效性和可行性。通过平面框架单元损伤识别算例分析,表明该方法是实用可行的。     

双基地雷达抗干扰模型的研究

从双基地雷达方程和实施压制性噪声干扰前后所带来的热噪声的变化出发,给出了双基地雷达探测区和干扰暴露区的计算模型,分析计算了在自卫式干扰和远距离支援干扰条件下的双基地雷达抗有源压制性干扰性能,并与单基地雷达情况进行了比较,说明收发分置的双基地体制雷达具有较强的抗干扰能力。给出了仿真算例,结果验证了这种观点。     

导弹装备战场损伤预测仿真研究

装备的战场损伤、损耗预测是作战保障的基础。文中构建了导弹装备损伤预测的马尔可夫Markov模型,导弹装备战场损伤部件数量动力学预测模型,并针对战场损伤强度和维修强度对损伤概率和部件损伤数量进行了仿真。对导弹作战计划以及装备保障与维修计划的制定具有指导意义。     

Fully sequential indifference‐zone selection procedures with variance‐dependent sampling

Fully sequential indifference‐zone selection procedures have been proposed in the simulation literature to select the system with the best mean performance from a group of simulated systems. However, the existing sequential indifference‐zone procedures allocate an equal number of samples to the two systems in comparison even if their variances are drastically different. In this paper we propose new fully sequential indifference‐zone procedures that allocate samples according to the variances. We show that the procedures work better than several existing sequential indifference‐zone procedures when variances of the systems are different. © 2006 Wiley Periodicals, Inc. Naval Research Logistics, 2006     

Simulation on the dynamic stability derivatives of battle-structure-damaged aircrafts

Accurately evaluating the aerodynamic performance of a battle-structure-damaged aircraft is essential to enable the pilot to optimize the flight control strategy. Based on CFD and rigid dynamic mesh techniques, a numerical method is developed to calculate the longitudinal and longitudinal-lateral coupling forces and moments with small amplitude sinusoidal pitch oscillation, and the corresponding dynamic de-rivatives of two fragment-structure-damaged and two continuous-rod-damaged models modified from the SACCON UAV. The results indicate that, at the reference point set in this paper, additional positive damping is generated in fragment-damaged configurations; thus, the absolute values of the negative pitch dynamic derivative increase. The missing wingtip induces negative pitch damping on the aircraft and decreases the value of the pitch dynamic derivative. The missing middle wing causes a noticeable increase in the absolute value of the pitch dynamic derivative;the missing parts on the right wing cause the aircraft to roll to the right side in the dynamic process, and the pitch-roll coupling cross dynamic derivatives are positive. Moreover, the values of these derivatives increase as the damaged area on the right wing increases, and an optimal case with the smallest cross dynamic derivative can be found to help improve the survivability of damaged aircraft.     

火灾场钢筋混凝土简支梁抗弯性能分析

通过对火灾中钢筋混凝土简支梁截面温度场和材料热力学性能分析,将混凝土分为弹性区和塑性区来分别计算其强度,建立了火灾场简支梁截面内混凝土应力和梁极限抗弯承载力的计算公式,通过具体算例分析了钢筋混凝土简支梁截面温度场和极限承载力的变化规律和原因。     

ESD与方波脉冲对集成电路注入损伤的比较研究

采用方波脉冲和ESD脉冲对3种集成电路进行了注入损伤效应实验,目的是比较二者对器件损伤的异同之处。分析时,首先对实验数据作拟合分析,建立起相关的数学模型,然后将模型值和实际值进行比较。可得到结论:实验器件有高压强场致PN结击穿和热效应2种损伤模式。对同一种器件,2种注入方式下的损伤模式相同或类似。方波注入下,各损伤阈值参数可拟合为1个式子来描述它们之间的关系,ESD注入下则还不确定;对同一器件,不同注入方式下的阈值不同,目前结果表明相差2~3倍。     

城市火灾危害的多因素灰色关联度研究

在对城市火灾危害的主要因素分析的基础上,应用灰色关联度分析方法,归纳了不同火灾风险因素对城市火灾危害性的影响程度,通过对灰色关联度的计算,对不同因素的火灾危害性进行了排序。     

模糊综合评判在战斗损伤评估中的应用

应用模糊综合评判对某型火炮的试验数据进行了初步分析,通过聚类分析得出了该型火炮的易损部件(战斗损伤),以及参加试验的6门火炮的损伤等级。计算结果表明,在战损评估中应用模糊数学的方法是可行的。