基于频率选择表面的雷达天线隐身应用研究

降低雷达天线的RCS而又保证雷达自身正常工作已成为目标隐身技术中的一个关键课题。介绍了由十字型振子单元构成的带阻式频率选择表面(FSS)的选频特性,探讨了FSS在低RCS抛物面天线和低RCS卡塞格伦天线中的工程应用,分析了应用于主、副反射面天线的隐身性能,最后得出2点结论,并指出在副反射面天线的工程应用中更容易实现。     

基于图像处理技术的定向管平行度测量

基于图像处理技术,探讨了一种火箭炮定向管平行度的测量方法,论述了该方法的测量原理和图像预处理过程中的图像增强、二值处理、边缘提取和几何校正等处理方法,给出了定向管平行度误差的计算方法。     

基于B-样条分形插值的垂直尺度因子的计算方法

将线性分形插值推广到B-样条上,可避免线性分形插值局限性,进一步扩大分形理论的应用范围。分形插值应用的关键问题,是如何合理地确定垂直尺度因子di的值,而它的计算却没有一种很有效的方法。通过解析方法,获得了均匀B-样条分形插值“S”点的代数解,从而,可准确计算出垂直尺度因子,解决了影响B-样条分形插值应用的难题。     

太赫兹粗糙金属目标镜面雷达散射截面预估方法

在太赫兹频段,研究金属目标表面粗糙度对雷达散射截面(Radar Cross Section,RCS)的调制作用,对粗糙金属目标的RCS缩比测量具有重要意义.通过研究太赫兹粗糙金属目标镜面RCS随粗糙度的变化规律,结合相干、非相干散射理论,在基尔霍夫近似法的基础上,提出一种特定参数区间粗糙金属目标镜面RCS的预估方法,并...     

C4ISR/M&S互操作HLA仿真设施

基于仿真互操作标准组织(Simulation Interoperability Standards Organization,SISO)C4ISR/M&S互操作技术参考模型和高层体系结构(High Level Architecture,HLA),C4ISR/M&S互操作HLA仿真设施为架构仿真系统运行体系提出了面向方面框架(Aspect Oriented Framework,AOF)和应用服务平台的技术.AOF能控制C4ISR/M&S互操作所引起的仿真系统结构复杂化,应用服务平台则能丰富仿真系统的运行环境,仿真设施可作为仿真系统通用运行体系的基础组件,支持复杂互操作系统开发.     

纳米Al2O3／聚酰亚胺耐高温应急粘接堵漏材料的研究

研究了纳米Al2O3粒子对聚酰亚胺粘接材料性能的影响.结果表明,纳米Al2O3粒子能明显提升聚酰亚胺粘接堵漏材料的粘接性能.当纳米Al2O3粒子添加量为8%～12%时,聚酰亚胺粘接堵漏材料的剪切强度可提高37%;纳米Al2O3/聚酰亚胺粘接堵漏材料在高温固化过程中,纳米Al2O3产生向粘接界面偏析现象.     

Electronic warfare in the optical band: Main features,examples and selected measurement data

The paper presents the possibilities of, and methods for, acquiring, analysing and processing optical signals in order to recognise, identify and counteract threats on the contemporary battleground. The main ways electronic warfare is waged in the optical band of the electromagnetic wave spectrum have been formulated, including the acquisition of optical emitter signatures, as well as ultraviolet (UV) and thermal (IR) signatures. The physical parameters and values describing the emission of laser radiation are discussed, including their importance in terms of creating optical signatures. Moreover, it has been shown that in the transformation of optical signals into signatures, only their spectral and temporal parameters can be applied. This was confirmed in experimental part of the paper, which includes our own measurements of spectral and temporal emission characteristics for three types of binocular laser rangefinders. It has been further shown that through simple registration and quick analysis involving comparison of emission time parameters in the case of UV signatures in “solar-blind” band, various events can be identified quickly and faultlessly. The same is true for IR signatures, where the amplitudes of the recorded signal for several wavelengths are compared. This was confirmed experimentally for UV signatures by registering and then analyzing signals from several events during military exercises at a training ground, namely Rocket Propelled Grenade (RPG) launches and explosions after hitting targets, trinitrotoluene (TNT) explosions, firing armour-piercing, fin-stabilised, discarding sabots (APFSDS) or high explosive (HE) projectiles. The final section describes a proposed model database of emitters, created as a result of analysing and transforming the recorded signals into optical signatures.     

Simulation on the dynamic stability derivatives of battle-structure-damaged aircrafts

Accurately evaluating the aerodynamic performance of a battle-structure-damaged aircraft is essential to enable the pilot to optimize the flight control strategy. Based on CFD and rigid dynamic mesh techniques, a numerical method is developed to calculate the longitudinal and longitudinal-lateral coupling forces and moments with small amplitude sinusoidal pitch oscillation, and the corresponding dynamic de-rivatives of two fragment-structure-damaged and two continuous-rod-damaged models modified from the SACCON UAV. The results indicate that, at the reference point set in this paper, additional positive damping is generated in fragment-damaged configurations; thus, the absolute values of the negative pitch dynamic derivative increase. The missing wingtip induces negative pitch damping on the aircraft and decreases the value of the pitch dynamic derivative. The missing middle wing causes a noticeable increase in the absolute value of the pitch dynamic derivative;the missing parts on the right wing cause the aircraft to roll to the right side in the dynamic process, and the pitch-roll coupling cross dynamic derivatives are positive. Moreover, the values of these derivatives increase as the damaged area on the right wing increases, and an optimal case with the smallest cross dynamic derivative can be found to help improve the survivability of damaged aircraft.     

测控站布局对区域卫星导航系统的影响

建立区域卫星导航系统的测控网是卫星导航系统要解决的关键问题之一。讨论国内测控站的布设问题,采用网格计算方法分析国内测控站对导航星座的可观测性。引入位置精度衰减因子PDOP和定轨中的法矩阵条件数,分析测控网对导航星座的观测几何结构强度以及测站位置分布对轨道确定精度的影响,仿真结果表明,利用我国有限的国土跨度和航天测控资源可以确保对导航卫星的测控任务的完成。对在国外布设测控站进行讨论和仿真,结果说明位于国外的测控站(如可在澳大利亚的珀斯设站)的加入能明显改善观测的几何结构强度、提高导航卫星的轨道精度。     

便携式防空导弹舵面偏转运动对比研究

建立了便携式防空导弹舵面偏转运动的数学模型,包括正弦偏转运动、不带零位脉冲调宽偏转运动和带零位脉冲调宽偏转运动,推导了相应的等效舵偏角矢量的公式,对比了3种舵面偏转运动对导弹性能的影响,所得结果对导弹设计中舵机的选取有参考价值。