卫星预警探测仿真模型研究

卫星预警探测系统对弹道导弹防御作战有重要影响.在分析卫星预警探测仿真模型的结构组成、运行机制和功能原理的基础上,构建了卫星预警探测仿真模型,并对构建内容进行了阐述.通过建立目标红外信号仿真数据表和背景大气辐射信号仿真数据表,提出了一种简单实用、操作性强的信噪比检测计算方法.最后,对模型进行了验证分析.仿真结果验证了卫星预警探测仿真模型探测弹道导弹目标的有效性和可行性.构建的模型可用于战争模拟系统中的导弹防御作战仿真.     

信息系统需求建模方法研究

在需求工程领域中,基于场景的需求建模方法越来越多地被人们采用.根据信息系统自身的特点和基于场景需求建模方法的优点,给出了一种基于场景的信息系统需求建模的具体方法.通过对雷达技术保障信息系统需求建模过程的实例分析,证明该方法能够快速、准确、全面地获取信息系统的需求模型,具有较高的应用价值.     

复杂电磁环境下作战仿真系统指挥控制体系建模

复杂电磁环境是信息化战争的重要特征,指挥控制体系是作战体系的"中枢".提出基于信息衍化的复杂电磁环境下作战仿真系统指挥控制体系的建模方法,研究了复杂电磁环境下作战仿真系统的模型体系分析了指挥控制体系的关系,建立了初步的指挥控制体质模型.为复杂电磁环境下作战体系建模与仿真打下一定的理论与模型基础.     

舰船磁场信号的频域分析

本文采用修正的周期图法(Welch法)对舰船磁场信号进行了功率谱估计并给出归一化曲线。在此基础上,提取了频域特征量,利用特征频率f_H进行了目标舰船速度的识别研究。计算机仿真表明,正识率可达95％以上。     

一种沉底水雷智能检查仪

为了完善经现代化改造的沉底水雷武器系统,而研制了一种集参数预置和引信检测为一体的智能检查仪。该仪器以单片机控制,具有智能化、便携、操作简单。人机交互良好等特点。它的应用方便了水雷参数的设定和仓库快速检测。     

相对论速度与双曲几何

本文试图将非欧几何之——双曲几何引入狭义相对论.结果表明,在一定的映射关系下,双曲坐标变换对应于相对论速度变换,双曲几何空间构成伪欧速度空间的等距浸入子空间.     

水雷磁引信目标识别技术初探

目标识别技术应用于水雷磁引信的关键是目标特征量的提取与分类器的设计。本文提出了舰船目标吨位识别的四维特征向量,设计出完整的二叉树分类器。仿真计算表明,这种特征量的正确识别率在90％以上,为目标识别技术在水雷磁引信中的应用作了有益的探索。     

Fabrication and characterization of Al-CuO nanocomposites prepared by sol-gel method

In this study, Al-CuO nanocomposites were fabricated by sol-gel method. As a contrast, the thermite was prepared by physical mixing at the equivalence ratio of 0.5, 1, 2, respectively. The intermediates and samples as prepared were characterized by SEM and XRD. The exothermic properties of the two samples prepared at different equivalence ratios were tested and the reaction products were characterized by XRD. The SEM results show that the sample prepared by the sol-gel method demonstrates a micron-sized agglomerated sphere formed by a mutual wrapping of Al NPs and CuO NPs, and the particles are evenly distributed in the agglomerate. In addition, when the content of Al powder is seriously insufficient, the heat release of the sample prepared by physical mixing is 1.6 times that of by sol-gel method. With the increase of Al powder content, the exothermic properties of Al/CuO NPs prepared by sol-gel method began to increase significantly compared with physical mixing and the difference is 1.5 times when the equivalence ratio increases to 2. It can be concluded that the reason for this result may be attributed to the different mass transfer modes of components due to the different morphologies of samples.     

Supercritical carbon dioxide as a new working medium for pneumatic launch: A theoretical study

Compared with the conventionally gaseous or liquid working media, the specific internal energy of supercritical carbon dioxide (SCD) is higher at the same temperature and pressure, and the critical temperature of carbon dioxide is close to room temperature, making SCD a potential new working medium for pneumatic launch. To analyze the feasibility of this conception, an analytical model of a pneumatic catapult is established on basis of the conservations of mass and energy. The model consists of a high-pressure chamber and a low-pressure chamber connected by multiple valves, and there is a movable piston in the low-pressure chamber that can push an aircraft to accelerate. The effects of the launch readiness state of SCD in the high-pressure chamber, the initial volume of the low-pressure chamber and the valve control on the movement of the aircraft are analyzed. It is found that there is a restrictive relation between the temperature and pressure of the launch readiness state of SCD, i.e., there is a maximum allowable launch readiness pressure when the launch readiness temperature is fixed. If this restrictive relation is not satisfied, the working medium in the low-pressure chamber will drop to its triple point within a few milliseconds, leading to a launch failure. Owing to this restrictive relation, there is an optimal launch readiness state of SCD with the highest working capacity for any allowable launch readiness temperature. The pressure of the low-pressure chamber will decrease significantly as the initial volume increases, leading to a decreased acceleration of the aircraft. The ac-celeration can be controlled below a critical value by a designed sequential blasting technique of multiple valves. The calculated results show that a 500 kg aircraft can be accelerated from 0 to 58 m/s in 0.9 s with 36 kg of carbon dioxide. This research provides a new technique for the controllable cold launch of an aircraft.     

排列熵算法的应用与发展

重点阐述了排列熵算法的基本原理,总结归纳了该算法在医学、生物和机械等领域的国内外研究和应用现状,最后展望了排列熵算法的未来发展趋势。研究表明：排列熵算法能够有效放大时间序列的微弱变化,且计算简单、实时性高,已在信号突变检测方面显示出良好的应用前景。