基于交叉熵最小化的 Turbo 码迭代译码停止准则

根据Turbo码最优译码算法及迭代译码的基本原理 ,在保证迭代收敛的条件下 ,利用交叉熵最小化原则推导出Turbo码译码过程中停止迭代的准则 ,并给出了一种降低计算复杂性和减少存贮空间的简化算法 ,最后通过仿真证明了此迭代停止准则及其简化算法的有效性。     

从故障特征群中快速确定故障点的方法

工程设备的结构日趋复杂,使故障诊断的难度不断增大。本文在最大故障信息量诊断的基础上提出了最大故障信息增量判断准则,可从故障特征群中一次找出最可能的故障点,简化了诊断过程,提高了诊断速度。     

液体火箭发动机燃烧不稳定性分析与热释放声放大机理

应用计算流体动力学方法对液体火箭发动机燃烧室内高频不稳定燃烧现象进行了数值仿真。气相方程用欧拉坐标系下的Ｎａｖｉｅｒ－Ｓｔｏｋｅｓ方程组描述,液相控制方程用Ｌａｇｒａｎｇｉａｎ坐标系下进行描述,湍流模型采用高雷诺数的ｋ－ε双方程模型。在燃烧室内加入正弦形脉冲扰动评定燃烧稳定性。引用Ｒａｙｌｅｉｇｈ热释放声放大机理对计算结果进行了分析,并对不同的扰动系数和液滴初始直径描出了燃烧稳定性极限图     

利用开源大数据的社会工作实时评估方法

鉴于目前社会工作评估评价方面的学术研究还较薄弱,存在无针对性指标体系,现有相关评比周期长、成本高等突出问题,探索构建了利用互联网开源大数据的实时定量评估模型,建立了针对性指标体系,提出评分快速计算方法,并设计实现原型软件。针对选定的社会工作进行案例实证,通过采集某省14个市州的互联网真实数据来评估其工作力度,结果与多位受访者的主观感受及相关官方评估基本相符,验证了所提模型的有效性和合理性。     

A study on the surface overpressure distribution and formation of a double curvature liner under a two-point initiation

The formation mechanism of an EFP(explosively formed projectile) using a double curvature liner under the overpressure effect generated by a regular oblique reflection was investigated in this paper.Based on the detonation wave propagation theory,the change of the incident angle of the detonation wave collision at different positions and the distribution area of the overpressure on the surface of the liner were calculated.Three-dimensional numerical simulations of the formation process of the EFP with tail as well as the ability to penetrate 45# steel were performed using LS-DYNA software,and the EFP ve-locity,the penetration ability,and the forming were assessed via experiments and x-ray photographs.The experimental results coincides with those of the simulations.Results indicate that the collision of the detonation wave was controlled to be a regular oblique reflection acting on the liner by setting the di-mensions of the unit charge and maintaining the pressure at the collision point region at more than 2.4 times the CJ detonation when the incident angle approached the critical angle.The distance from the liner midline to the boundary of the area within which the pressure ratio of the regular oblique reflection pressure to the CJ detonation pressure was greater than 2.5,2,and 1.5was approximately 0.66 mm,1.32 mm,and 3.3 mm,respectively.It is noted that pressure gradient caused the liner to turn inside out in the middle to form the head of the EFP and close the two tails of the EFP at approximately 120μs.The penetration depth of the EFP into a 45# steel target exceeded 30 mm,and there was radial expansion between the head and tail of the EFE increasing the penetration resistance of the EFP.Therefore,the structural size of the unit charge and the liner can be further optimized to reduce resistance to increase the penetration ability of the EFP.     

Shock initiation performance of NTO-based polymer bonded explosive

3-nitro-1,2,4-tri-azol-5-one (NTO) is a high energy insensitive explosive. To study the shock initiation process of NTO-based polymer bonded explosive JEOL-1 (32%octahydro-1,3,5,7-tetranitro-1,3,5,7-tetrazocine (HMX), 32% NTO, 28% Al and 8% binder system), the cylinder test, the gap experiments and numerical simulation were carried out. Firstly, we got the detonation velocity (7746 m/s) and the parameters of Jones-Wilkins-Lee (JWL) equation of state (EOS) for detonation product by cylinder test and numerical simulation. Secondly, the Hugoniot curve of unreacted explosive for JEOL-1 was obtained calculating the data of pressure and time at different Lagrangian positions. Then the JWL EOS of unreacted explosive was obtained by utilizing the Hugoniot curve as the reference curve. Finally, we got the pressure growth history of JEOL-1 under shock wave stimulation and the parameters of the ignition and growth reaction rate equation were obtained by the pressure-time curves measured by the shock-initiation gap experiment and numerical simulation. The determined trinomial ignition and growth model (IG model) parameters can be applied to subsequently simulation analysis and design of insensitive ammunition with NTO-based polymer bonded explosive.     

基于边扫描边跟踪系统的多目标航迹起始相关

系统地研究了基于边扫描边跟踪雷达系统中对多机动目标的航迹起始及点迹-航迹相关。航迹起始采用滑窗法,对于点迹-航迹相关,可将K近邻域法和NN算法结合应用。对该方法的航迹相关准则进行了详细的描述,并与NN算法和K近邻域法进行了比较。     

炸药装药在压剪加载下的起爆特点

进行了两类压剪加载实验：（１）利用石英的平面正碰撞产生压剪加载的实验,采用电磁质速法测试装药试件内部不同质点的运动情况,分析炸药装药中发生化学反应的可能性;（２）在压剪炮上采用平行倾斜碰撞产生压剪加载的实验,观测炸药装药爆炸的可能性。由实验可以看出：在亚爆轰状态的压缩加载应力条件下,剪切的联合作用对炸药的起爆起到敏化作用,适当比例的压剪加载造成更加敏感的炸药起爆响应。文中给出了起爆响应规律和响应机制的实验分析。     

热射流起爆过程的数值模拟

采用改进的化学非平衡流解耦方法处理Euler反应流方程,并以H2/air 9组分21方程模型对竖直喷注的热射流起爆过程进行了二维数值模拟。对流项采用五阶WENO离散格式,时间推进采用二阶Runge-Kutta方法。详细分析了热射流以不同速度、入射位置、入射宽度和入射倾角喷射时在爆震管内形成的流场,总结了射流参数状态影响起爆的一般规律;解释了激波、火焰的相互作用对"热点"的形成以及转变为爆震的影响,特别是激波反射对"热点"形成的促进作用。结果表明,爆震波通常由火焰面和固壁附近狭长未燃区域中的"热点"产生。"热点"向爆震波发展的过程是过驱爆震阶段,存在三波结构。为了实现快速起爆,应当增大射流入射速度、贴近侧壁并以适当入射角度喷射热射流。     

同时射击时反坦克导弹视场交叉数学模型研究

反坦克导弹同时射击时测角视场交叉可能引起导弹失控,针对此问题,利用信息系统的位置地理信息,参照装备的基本性能参数,构建了配置阵地的数学模型,得出了同时射击的可行性判据,为阵地射击指挥提供了决策支持。