试论智能建筑中火灾自动报警系统的性能化设计

概述了智能建筑的概念和火灾自动报警系统的关系,进而阐述了智能建筑中火灾自动报警系统要进行性能化设计的原因、方法和应着重注意的通信协议问题。     

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.     

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。     

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。     

激光测距仪故障自动检测系统的电路设计

针对手持式激光测距仪的复杂电路系统,设计了一套完整的自动检测电路,成功地解决了激光测距仪电路的故障诊断难题。     

并行环境下的管理信息系统开发模式研究

通过分析生命周期法、原型法等传统管理信息系统开发方法存在的一些不足之处,以及将并行工程的思想应用到管理信息系统的开发中,提出了一种基于并行环境下的管理信息系统开发模式,并结合装甲装备器材资源调度系统的开发,对这种并行环境开发模式进行了探讨和研究.     

超低轨道卫星摄动特性分析及轨道维持方法

针对超低轨道卫星长时间在轨飞行的轨道维持问题,分析了超低轨道平均偏心率矢量变化特性,提出了一种超低轨道维持的控制方法。分析了J2、J3摄动以及大气阻力摄动作用下超低轨道卫星偏心率矢量的变化特性;基于能量守恒原理设计了超低轨道高度维持的控制策略;通过仿真算例验证了控制策略的有效性。结果表明:在地球非球形引力摄动、大气阻力摄动和速度脉冲作用下超低轨道平均偏心率的变化是稳定的,所设计的轨道维持方法不仅能够实现超低轨道高度维持,确保平均偏心率矢量收敛至平衡位置,且用于轨道维持的燃料消耗合理,能够满足长时间的超低轨道飞行要求。     

Controllable combustion behaviors of the laser-controlled solid propellant

Microsatellites have been widely applied in the fields of communication,remote sensing,navigation and science exploration due to its characteristics of low cost,flexible launch mode and short development period.However,conventional solid-propellant have difficulties in starting and interrupting combustion because combustion is autonomously sustained after ignition.Herein,we proposed a new type of solid-propellant named laser-controlled solid propellant,which is sensitive to laser irradiation and can be started or interrupted by switching on/off the continuous wave laser.To demonstrate the feasibility and investigate the controllable combustion behaviors under different laser on/off conditions,the combus-tion parameters including burning rate,ignition delay time and platform pressure were tested using pressure sensor,high-speed camera and thermographic camera.The results showed that the increase of laser-on or laser-off duration both will lead to the decrease of propellant combustion performance during re-ignition and re-combustion process.This is mainly attributed to the laser attenuation caused by the accumulation of combustion residue and the change of chamber ambient temperature.Simultaneously,the multiple ignition tests revealed that the increased chamber ambient temperature after combustion can make up for the energy loss of laser attenuation and expansion of chamber cavity.However,the laser-controlled combustion performance of solid propellant displayed a decrease trend with the addi-tion of ignition times.Nevertheless,the results still exhibited good laser-controlled agility of laser-controlled solid propellant and manifested its inspiring potential in many aspects of space missions.     

Optimal inventory control policy for periodic‐review inventory systems with inventory‐level‐dependent demand

We consider a setting in which inventory plays both promotional and service roles; that is, higher inventories not only improve service levels but also stimulate demand by serving as a promotional tool (e.g., as the result of advertising effect by the enhanced product visibility). Specifically, we study the periodic‐review inventory systems in which the demand in each period is uncertain but increases with the inventory level. We investigate the multiperiod model with normal and expediting orders in each period, that is, any shortage will be met through emergency replenishment. Such a model takes the lost sales model as a special case. For the cases without and with fixed order costs, the optimal inventory replenishment policy is shown to be of the base‐stock type and of the (s,S) type, respectively. © 2012 Wiley Periodicals, Inc. Naval Research Logistics, 2012