Target Tracking of Fire-Control Radar on the Method of Intermittent Radiation

从火控雷达抗反辐射导弹的迫切需求出发,将间歇辐射理论应用于火控雷达,提出了间歇式目标跟踪方法.首先对间歇式跟踪原理进行了分析;其次,基于单脉冲技术分析了采样间隔的自适应变化原则,同时提出了跟踪性能的评价指标,并进一步对跟踪效果进行了仿真.结果证明间歇式目标跟踪方法可以同时实现对反辐射导弹载机的准确跟踪和对反辐射导弹的有效对抗.     

基于正弦高斯组合的UWB脉冲波形设计

针对美国FCC关于超宽带传输系统提出的辐射掩蔽特性,提出了一种基于正弦高斯组合的UWB脉冲波形设计新方案。以一组正弦高斯脉冲为基函数,利用最小均方误差准则(LSE)选取加权系数对基函数进行线性组合,通过调整基函数的载波频率和脉冲形成因子,对波形进一步优化。分析了TH-PPM UWB多用户系统的误码率性能。仿真结果表明,与高斯二阶微分脉冲、随机系数组合脉冲相比,基于正弦高斯组合脉冲具有更高的频谱利用率,误码性能更优。     

航天测控调度问题的拉格朗日启发式算法

通过分析航天测控调度问题的测控需求,建立了航天测控调度0-1整数规划模型,运用拉格朗日松弛方法对模型中的任务约束和设备约束进行了松弛,运用次梯度优化算法求得了航天测控调度问题上界,同时得到了决策变量对应的拉格朗日权重,可以作为决策变量在最优解中是否被调度的启发式信息,对拉格朗日权重进行分析,提出了求解问题可行解的拉格朗日启发式算法。最后,通过对两个场景的试验分析验证了拉格朗日启发式算法所求可行解的优越性。     

助推段反TBM装备发展构想

根据战术弹道导弹射程与助推段发动机关机高度和关机点距发射点斜距的关系,比较了2种周边国家和地区的战术弹道导弹助推段发动机关机数据,通过设想的反导武器,分析了对这2种战术弹道导弹拦截的可行性,结合可行性分析结果,提出助推段预警、指控、拦截等反导装备的发展构想。     

循迹智能小车的系统设计

系统采用AT89S52单片机作为控制核心,结合红外遥控电路、红外循迹避障电路和电机驱动电路等硬件组成智能小车,通过软件设计实现小车对行驶路线的智能循迹。设计中电机驱动采用L9110芯片,利用红外光的接受差值实现蔽障,能有效地控制其避免障碍物。用红外传感器TCRT5000来检测道路上的黑线,使单片机循迹控制小车按预定的速度行驶。可用遥控器遥控小车的运行状态,并可自由切换到自动运行模式。具有运行稳定、控制精度高等优点,在科技创新和科技推广方面有很好的应用前景。     

基于智慧校园建设推进军队院校教育现代化路径探究

教育信息化是教育现代化的基本内涵和显著特征。当前,我国正处于由基本实现教育现代化迈向整体实现教育现代化的重要战略期,国家教育从理论和实践层面进行了大量探索。在军队院校教育领域,教育技术应用、训练管理领域网络建设、数字校园建设等均为军队院校教育现代化奠定了创新发展基础,智能教育应用模式的改革探索也为军队院校教育现代化描绘了未来建设愿景。本文认为,推进军队院校教育现代化应发挥智慧校园建设平台的基础作用,充分融入国家教育体系,注重以先进教育理念驱动创新发展、以前沿信息技术提供解决方案、以总体架构设计规范目标功能、以智慧育人环境承载应用服务、以数据资源体系孕育智慧生态,走开军委军种院校三级联动推动创新发展的路子。     

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.     

基于遗传算法的航空兵出动架次计算方法

针对航空兵出动架次计算问题,基于资源受限项目调度理论进行问题描述和建模,以给定兵力对目标任务的最大出动架次为效能指标,分析影响因素和约束条件,建立了问题数学模型.根据问题模型特点,采用遗传算法进行求解,针对染色体编码问题,设计了一种扩展任务列表编码方法;针对初始解集求解问题,提出了一种基于优先规则的出动架次分配算法.并构建了航空兵出动架次计算仿真算例对问题模型和求解算法进行验证,实验结果表明,所提模型和算法能够有效求解大规模航空兵出动架次计算问题.     

CBM与IETM集成中的数据模型设计及运用

针对现有交互式电子手册(IETM-Interactive Electronic Technical Manual)与基于状态维修(CBM-Con-dition Based Maintenance)系统集成设计中对接口数据的特点类型、结构模式及运用过程缺乏规范化设计的不足,基于开放系统体系结构(OSA-CBM),对集成中的数据内容进行了统一建模,规范了OSA-CBM 6层数据类型与3级CBM系统、4种集成方式的相互关系.面向CBM与IETM集成应用,提出了3种数据结构模式及其运用过程,有效解决了集成接口中的数据模型设计问题.     

Economic screening procedures using a correlated variable with multidecision alternatives

Economic screening procedures using a correlated variable are developed for selecting markets in situations when there are several markets with different profit/ cost structures. It is assumed that the performance variable and the screening variable are jointly normally distributed. Profit models are constructed which involve three profit/cost components: profit from a conforming item, cost from an accepted nonconforming item, and screening inspection cost. Methods of finding the optimal screening procedures are presented and numerical examples are given.