基于子协方差阵加权的三星时差定位数据综合

为提高三星时差定位系统的定位精度,需要将系统在不同时间得到的多个定位估计结果进行统计综合。本文提出了一种基于子协方差阵加权的定位数据综合算法。该算法根据单点定位精度分析结果,先利用定位误差协方差的二维子阵的逆矩阵作为权矩阵,通过加权最小二乘估计目标空间三维坐标位置中的其中两维,再利用WGS-84地球模型求解另一维坐标。仿真实验表明,相比已有算法,所提新算法可以明显提高定位精度。     

一种基于解析冗余关系的半定性故障隔离方法在航天器推进系统中的应用

针对航天器推进系统的时变特性以及随机因素给故障隔离带来的困难,提出了基于Z-检验分析和解析冗余关系相结合的半定性故障隔离方法。基于状态空间转换的思想,运用基于系统诊断键合图模型建立的解析冗余关系挖掘系统时不变的结构特征空间信息,并对解析冗余关系残差进行趋势分析获取时不变、具有残差变化方向的故障特征矩阵,针对存在随机因素对残差定性化的影响,利用了Z-检验分析对残差进行定性化获取观察特征,通过观测特征与故障特征的比较进行系统故障隔离。将该方法应用于推进系统的故障隔离中,结果证明了该方法能有效避免获取推进系统时变诊断准则以及来自系统建模和参数测量等随机因素的干扰,提高了推进系统故障隔离的鲁棒性。     

一种基于UML/OCL的软件测试方法

根据UML/OCL和建模环境提供的软件模型信息,以一个武器装备管理信息系统的装备入库顺序图为例,在分析UML/OCL顺序图的语法和对象间的交互信息的基础上产生测试场景,提供了一种基于UML/OCL的面向对象的软件测试方法,并提出测试自动化的设想,对软件测试有一定的借鉴作用。     

网络雷达对抗系统的相控阵雷达波束扫描分析

针对相控阵雷达波束扫描的捷变特性,提出了基于网络雷达对抗系统的波束扫描分析方法。由于各侦察子系统空间分布特性不同,网络雷达对抗系统所获得的相控阵雷达波束指向判决各不相同。结合DS证据理论,将各个侦察子系统的判决结果融合处理,可有效消除不确定信息,提高波束扫描的判决准确率。通过仿真试验,验证了该方法的有效性和可行性。     

应用UIO的卫星姿控故障检测与仿真

为了克服未知输入对观测器的影响,防止在故障检测滤波器中出现错误的报警,以Chen和Patton提出的未知输入观测器的基本架构,设计了两个观测器.这两个观测器分别对故障敏感和不敏感,推导了两种情况下的误差方程,并且设计了残差.该残差能够与故障信号建立直接的联系,便于对故障的分析与诊断.该方法用于卫星姿控系统中,并且进行了仿真.     

陶瓷基复合装甲防12.7mm穿甲燃烧弹的靶试研究（Ⅱ）

基于对材料特性和防弹机理的认识,设计了由（SiC＋Si）陶瓷、616装甲钢和高强PE材料构成的陶瓷基复合靶板,靶板防护面密度为118 kg/m2,尺寸为500 mm×500 mm×25 mm。利用现役12.7 mm穿甲燃烧弹考核靶板在6发弹打击下的防护能力,检验靶板设计思路。结果表明：靶板结构是可行的,可防住V25为818 m/s的现役12.7 mm穿甲燃烧弹。     

基于禁忌搜索的作战重心分析与选择方法

研究了作战目标网络的重心分析与选择方法,为战场指挥员的指挥决策提供依据.定义了战场重心的概念,从考虑打击代价的角度建立重心发现的优化模型,给出了基于禁忌搜索的求解算法,并通过实验案例验证了模型和算法的有效性和可行性.     

设备健康状态评估指标体系约简方法

针对设备健康状态评估涉及指标多、指标间关系复杂的问题,提出基于粗糙集和遗传算法的设备健康状态评估指标体系约简方法.将粗糙集理论和遗传算法相结合,对设备健康状态评估指标进行约简的同时,提高约简效率.某燃气轮机健康状态评估指标体系约简案例显示,该方法能够在不失代表性、系统性的前提下,将复杂指标体系约简为较为简洁、明了的指标体系,保持评估结果准确的同时减少信息收集工作量.     

Shock-induced reaction behaviors of functionally graded reactive material

In this paper, the ballistic impact experiments, including impact test chamber and impact double-spaced plates, were conducted to study the reaction behaviors of a novel functionally graded reactive material (FGRM), which was composed of polytetrafluoroethylene/aluminum (PTFE/Al) and PTFE/Al/bismuth trioxide (Bi₂O₃). The experiments showed that the impact direction of the FGRM had a significant effect on the reaction. With the same impact velocity, when the first impact material was PTFE/Al/Bi₂O₃, compared with first impact material PTFE/Al, the FGRM induced higher overpressure in the test chamber and larger damaged area of double-spaced plates. The theoretical model, which considered the shock wave generation and propagation, the effect of the shock wave on reaction efficiency, and penetration behaviors, was developed to analyze the reaction behaviors of the FGRM. The model predicted first impact material of the FGRM with a higher shock impedance was conducive to the reaction of reactive materials. The conclusion of this study provides significant information about the design and application of reactive materials.     

Influence of a liquid-filled compartment structure on the incoming shaped charge jet stability

Liquid-filled compartment structure consists of a bulk steel plate with matrix blind holes which are filled with liquid and a steel front plate to seal up the liquid with rings and bolts.The liquid-filled compart-ment structure can resist the shaped charge warhead effectively.This paper presents experimental and theoretical investigations of the penetration ability of the residual shaped charge jet emerging from the liquid-filled compartment structure after the penetration process at different impact angles.On the basis of shock wave propagation theory,the influence of the liquid-filled compartment structure on jet sta-bility is analysed.The interferences of the liquid backflow caused by a reflected shock wave and a back plate on jet stability under different impact angles are also examined.In addition,the range of the disturbed velocity segments of the jet at different impact angles and the penetration ability of the re-sidual jet are obtained.A theoretical model is validated against the experimental penetration depths.