Lorentz序列空间光滑性

给出了Lorentz序列空间光滑性的判据,论证了当P>1时d(w,p)是局部光滑的。     

线性赋范空间中一类非线性方程的迭代解

在一般的线性赋范空间中研究一类算子方程的解的迭代逼近问题,获得了一系列结果。     

语音信号相空间重构中时间延迟选择的改进的平均位移法

本文在分析时间序列相空间重构中的时间延迟选取的平均位移法基础上,对该法的原有度量进行改进,得到较好的求时间延迟的准则。改进的平均位移法具有更强的理论依据;应用于语音信号相空间重构的仿真实验表明,其度量一般情况下可得到合适的时间延迟。     

傅立叶级数型导弹工作式研究

空空导弹弹道计算需要解算一组复杂的微分方程。火控系统为了解算导弹的攻击区,不能直接采用这组微分方程,必须事先建立一套简单可行的导弹工作式,它既要满足火控系统的要求,又要充分地发挥出导弹的作用,满足一定的误差要求。笔者阐述了如何为空空导弹的发射建立一种全向攻击的工作式。     

美国太空安全领域最新发展分析

美国认为太空已被普遍认定为最重要的作战域之一,未来的太空安全态势将愈发严峻。本文认为, 美国正面向未来太空对抗环境进行全面转型, 从顶层战略、作战理论、组织结构、战备训练、装备技术等方面开展研究、调整和长远布局, 如以我为主要对手谋划布局、发布系列军事航天顶层指导文件、大幅增加太空攻防作战相关经费投入等。 目前, 美军正处于新旧体系转换、 下一代能力构建发展的关键期, 不仅正在变革军队组织体制、重组太空攻防作战力量, 还积极开展系列演习演训, 以加速形成太空攻防实战能力。美军这一系列动向将对未来太空领域安全与发展产生重大影响, 应引起我高度重视。     

【专题】装备保障数据中心体系结构设计

数据中心作为支撑装备保障指挥、管理、维修、供应及训练等业务运行的重要基础,是数据交换的枢纽和各级数据的总汇,也是信息服务的中心,对深化装备保障信息需求、实现保障信息有效管理和强化保障信息综合应用至关重要。本文面向装备保障数据中心建设需求,分析了装备保障数据中心的内涵及其在数据汇聚存储、数据共享交换、保障决策支持及综合信息服务等方面的重要作用,从总体架构、物理结构和数据结构三个方面开展了数据中心体系结构设计;同时,立足装备保障数据中心建设与应用,针对应该重点把握的数据标准规范建设、配套数据采集手段、加强安全保密建设、完善运维管理体系及建立专业分析团队等问题进行了阐述。研究成果可为实际开展装备保障数据中心建设提供 参考。     

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.     

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.     

基于公共燃气排导结构的共架发射系统武器选择与布局方法

公共燃气排导结构和同心筒结构的共架发射系统由于燃气排导机理不同,其对武器发射的影响及在武器选择、布局等方面均存在较大差异.针对公共燃气排导结构的共架发射系统分析了公共燃气排导对武器发射的影响,提出了武器选择与布局方法,通过算例进行了验证并得出结论:公共燃气排导结构的共架发射系统武器布局上应采取分散布局,武器选择上应优先选择“无发射活动、对应武器数量较多、烧蚀值较小”的模块,且按照模块编号依次交替在不同模块进行武器发射.     

舰载无人机对岸可观测安全飞行空间分析模型

基于舰载无人机对岸上目标的观测能力出发研究出的"理想观参",考虑各种因素对舰载无人机在任务区域飞行安全的影响,建立了地理通视性分析模型、地理可飞性分析模型、飞行可控性分析模型、弹道安全性分析模型和观参上限分析模型;综合上述模型,给出了舰载无人机可观测安全飞行空间,满足可观测安全飞行空间的观测参数即为当前环境下的"实用观参";根据本文模型研制的舰载无人机对岸射击观测辅助决策软件,实现了舰载无人机对岸射击观测的科学决策。