高精度频率分辨在振动信号辨识中的应用

发动机振动信号处理通常采用DASP软件进行。由于软件功能限制,DASP处理采样频率为50 kHz发动机振动信号时,频谱的频率分辨率最高精度仅为12.2 Hz,导致对微弱及故障信号的辨识较为困难。本文采用抗混叠低通滤波、信号抽取及短时傅里叶变换相结合的信号分析方法,有效提高了频率分辨率的精度,最高精度达到1.2 Hz,达到了理想的频率辨识效果。     

Experimental study on ceramic membrane technology for onboard oxygen generation

The ceramic membrane oxygen generation technology has advantages of high concentra-tion of produced oxygen and potential nuclear and biochemical protection capability. The present paper studies the ceramic membrane technology for onboard oxygen generation. Comparisons are made to have knowledge of the effects of two kinds of ceramic membrane separation technologies on oxygen generation, namely electricity driven ceramic membrane separation oxygen generation technology (EDCMSOGT) and pressure driven ceramic membrane separation oxygen generation technology (PDCMSOGT). Experiments were conducted under different temperatures, pressures of feed air and produced oxygen flow rates. On the basis of these experiments, the flow rate of feed air, electric power provided, oxygen recovery rate and concentration of produced oxygen are compared under each working condition. It is concluded that the EDCMSOGT is the oxygen generation means more suitable for onboard conditions.     

基于目标管理的大学生涯规划设计探析

目标管理是20世纪50年代中期,在科学管理和行为管理理论基础上形成的一套管理理论,是现代化管理的一项重要内容.本文将目标管理理论应用于大学生涯规划设计,主要从大学生涯规划设计的内涵、意义、主要内容和有效途径探讨了大学生涯规划设计,以便解决大学新生入学后的目标缺失问题.     

一种基于更动影响域分析的回归测试方法

为减少回归测试成本、提高效率,提出了一种基于更动影响域分析的回归测试方法,详细说明了更动类型,并针对每种类型提出了对应的影响域分析策略.研究表明,该方法技术指导性好,易使用,提高了回归测试的充分性,进一步保证了测试质量.     

精确对抗技术的现状及其发展

多次战争表明,精确制导武器是决定性胜利的关键武器。精确制导武器的核心是精确制导系统,而精确对抗的核心就是精确对抗精确制导系统。简要介绍美国红外精确对抗装备及其试验,从电子战的角度只讨论空地和空空红外制导导弹的精确对抗问题。     

Wimax密码算法使用模式的探讨

目前，Wimax凭借其宽带高速的优点已经成为3G的一个标准，在无线城域网中拥有广阔的应用前景。同时，Wimax的安全问题也不客忽视，正受到越来越多人的研究，但对于密码算法使用模式的研究较少。文章重点介绍了Wimax安全子层中密码算法的三种主要使用模式（密码块链接模式、计数器模式和MAC层密码链接一计数器模式），并对它们的优缺点进行了比较分析。     

Hybrid Simulation System Study of SINS/CNS Integrated Navigation

In flight tests, to demonstrate the performance of integrated navigation systems, which are strapdown inertial navigation systems/celestial navigation systems (SINS/CNS), will involve a lot of effort and a heavy financial budget. So, it is important to design a functional self-contained hardware in a loop simulation system on the ground for solving the verification of SINS/CNS integrated navigation systems. Aiming at solving the main program, a high precision, versatile and better real-time performance hybrid simulation system of SINS/CNS integrated navigation is presented. The system adopts the design of hardware-functional modularization and software-flow integration, and makes use of a trajectory generator to produce simulated nominal trajectory data which is a uniform reference to signal process, and employs unique time synchronization algorithms to collect actual errors data of inertial sub-system and celestial sub-system. By combining with nominal trajectory data, the data smoothing, all-sky autonomous star map identification and integrated navigation algorithm based on unscented Kalman filtering (UKF), this system can accomplish a lot of system performance testing. It has the features of flexibility and extensibility and can be used to effectively reduce the experimental expense and shorten the development time of integrated navigation system, which is significant for studying algorithm performance, system speciality, and practical application of integrated navigation system.     

ECK2007模型与其他密钥协商协议模型安全强弱关系的形式化证明

比较了安全性模型Extended Canetti＆Krawczyk 2007（ECK 2007）与其他4个安全模型（Bellare＆Rogaway 1993（BR93）,Bellare＆Rogaway 1995（BR95）,Bellare,Pointcheval＆Rogaway 2000（BPR 2000）和Canetti＆Krawczyk 2001（CK2001））的不同点,并形式化地分析了这些模型之间的强弱关系,对模型间存在的蕴含关系提供了形式化证明,对非蕴含关系提供了反例。     

Achievements of Space Scientific Experiments Aboard SJ-8 Satellite

As scientific experiment payloads, microgravity experiments of fluid physics, life science,combustion science, physics and accelerator measurement were conducted on board the Chinese recoverable satellite SJ-8 during 18-day orbital flight. The experimental payloads and an experiment support system constituted the microgravity experiment system of the flight mission. This article has presented the briefs of the scientific achievements of these space experiments, the composition and performance of the Microgravity Experimental System (MES) and the general picture of the overall flight mission, respectively.      

基于可观测度分析和模型预测的空间自标定方法

光纤陀螺以其优点适合空间飞行器定姿要求,但长期在轨飞行必须对光纤陀螺进行自标定。通常采用高维复杂陀螺模型计算实时性误差,而采用舍去状态量的降维模型影响系统定姿精度。针对这一问题,通过星敏感器观测,对高维陀螺模型进行可观测度分析,提出了一种基于模型预测的降维模型,将可观测度较低的状态作为模型误差进行预测估计,保证了系统精度并大大减小了计算量。半物理仿真结果表明此算法精度略高于高维模型自标定方法,计算量仅为高维模型的1/10,显著提高了系统的实时性。