基于多种评价方法的储油库风险评价研究

不同的安全评价方法各有其应用优点和不足,实践表明将多种方法综合应用将取得较好的安全评价效果。以中国石油某商业储备库为研究对象,针对不同的评价单元,基于不同评价方法的特点与优势,采用安全检查表法、预先危险性分析法、美国道化学方法、易燃易爆重大危险源伤害模型评价法、事故树法、作业条件危险性评价法6种方法对该油库系统深入地进行了安全评价及危险性分析,并对评价结果进行了分析比较。在此基础上,提出了储油库设计建设及日常运营过程中应采用（取）的安全设施和安全措施,为储油库的安全设计、施工及安全运营奠定了坚实的基础。     

Influence of multiple structural parameters on interior ballistics based on orthogonal test methods

Influence of multiple structural parameters on the performance of a gun launch system driven by high-pressure reactive gases is important for structural design and performance adjustment. A coupled lumped parameter model was utilized to predict the propellant combustion, and a dynamic finite element method was applied to approximate the mechanical interactions between the projectile and the barrel. The combustion and the mechanical interactions were coupled through a user subroutine interface in ABAQUS. The correctness and the capability of the finite element approximations in capturing small structural changes were validated by comparing predicted resistance with experiments. Based on the coupled model, the influence of structural parameters of a medium-caliber gun on the system performance was investigated. In order to reduce the research costs, orthogonal tests were designed to investigate the comprehensive effects of the parameters. According to statistical analysis, the important order of the structural parameters on the launching process was obtained. The results indicate that the influence of the width of the rotating band stands out among the studied parameters in the gun. The work provides a method to investigate the influence of multiple parameters on system performance and gives guidance for controlling the system performance.     

电子可编程模拟器件 IMP50E30 特性及其应用

详细介绍了电子可编程模拟器件（ＥＰＡＣ）的主要技术特点及其典型芯片ＩＭＰ５０Ｅ３０,并给出了它在多路测量中的应用实例．     

单兵数字化系统外部通信研究——“数字化战场与单兵数字化系统”系列论文之六

讨论了单兵数字化系统外部通信的功能结构和实现途径，以及战场信息网的无线电网和地域网实现。重点研究了联合战术信息分布系统ＪＴＩＤＳ，包括其ＴＤＭＡ工作方式和多网工作原理。最后研究了单兵数字化系统通信的一个安全问题。     

网络公开军事情报工作探析

随着信息技术的迅猛发展,互联网已深刻融入人们生产生活全过程,这使得网络中留下了各组织、机构和人员活动的海量信息痕迹。借助云计算、大数据等网络信息技术,这些信息痕迹已逐渐成为各国军事情报部门重要的情报来源,围绕网络空间展开的军事情报与反情报斗争日益激烈,需要引起高度重视。     

均匀裸堆单组扩散方程的普遍解及其分析

在现行核反应堆理论文献中,对有奇异源时中子扩散方程的解讨论甚少,本文对此作了补充,并给出普遍解公式。这对于深入了解有奇异源时堆的临界行为和中子通量的时空特性,以及堆在次临界启动时的物理性能,均具有重要的参考价值。     

独立分量分析在液体火箭发动机故障检测中的应用

针对液体火箭发动机试车中,因噪声干扰、不同源信号之间的混叠而造成的信号信噪比低、信号分析和特征提取难度大的问题,提出采用独立分量分析(ICA)法对液体火箭发动机试车信号进行分离,以提高信号的信噪比,并能实时反映各子系统工作过程,为数据分析、特征提取和故障检测与诊断提供可靠的信号。通过对某型液体火箭发动机热试车压强信号进行实例分析,验证了该方法的有效性。     

单一来源同类装备价格形成机制存在的问题及对策

近年来,随着国防和军队全面深化改革的深入推进和装备建设的快速发展,装备价格管理工作的重要性不断提升,但军队目前承担的装备审价任务日趋繁重,存量不减、增量日增等新情况和新问题给装备价格管理工作带来了新挑战。本文以单一来源同类装备为研究对象,借鉴《军品定价议价规则(试行)》中竞争议价和征询议价不审价的原理,从单一来源同类装备价格的形成主体、装备审价任务量、装备价格的测算方法、装备价格的形成过程以及装备价格的影响因素等五个方面分析了价格形成机制存在的问题,并从主观因素和客观因素两方面探讨了存在问题的原因,提出应在明确价格形成主体的职能权限、科学确定价格的测算方法、完善价格法律法规、建设价格数据平台、加强价格人才队伍建设等方向优化单一来源同类装备价格形成机制的对策建议。     

Robust cubature Kalman filter method for the nonlinear alignment of SINS

Nonlinear initial alignment is a significant research topic for strapdown inertial navigation system(SINS).Cubature Kalman filter(CKF)is a popular tool for nonlinear initial alignment.Standard CKF assumes that the statics of the observation noise are pre-given before the filtering process.Therefore,any unpredicted outliers in observation noise will decrease the stability of the filter.In view of this problem,improved CKF method with robustness is proposed.Multiple fading factors are introduced to rescale the obser-vation noise covariance.Then the update stage of the filter can be autonomously tuned,and if there are outliers exist in the observations,the update should be less weighted.Under the Gaussian assumption of KF,the Mahalanobis distance of the innovation vector is supposed to be Chi-square distributed.Therefore a judging index based on Chi-square test is designed to detect the noise outliers,determining whether the fading tune are required.The proposed method is applied in the nonlinear alignment of SINS,and vehicle experiment proves the effective of the proposed method.     

A novel launch dynamics measurement system for multiple launch rocket system and comparative analysis with numerical simulations

In this paper,a novel launch dynamics measurement system based on the photoelectric sensor pair is built.The actual muzzle time(i.e.a time duration that originates from the initial movement to the rocket's departure from the muzzle)and the muzzle velocity are measured.Compared with the classical methods,the actual muzzle time is obtained by eliminating the ignition delay.The comparative analysis method is proposed with numerical simulations established by the transfer matrix method for multibody systems.The experiment results indicate that the proposed measurement system can effectively measure the actual muzzle time and reduce the error of classical methods,which match well with the simulation results showing the launch dynamics model is reliable and helpful for further analysis and design of the MLRS.