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雷达目标低频RCS可视化计算 总被引:1,自引:0,他引:1
随着计算机进一步发展,科学计算可视化越来越受到重视;而适用于低频区RCS(雷达散射截面)计算的传统方法MOM(矩量法),也越来越显示其价值;为了方便电磁计算和电磁建模,基于先进的计算机三维造型技术和可视化编程手段,采用回路线栅矩量法,计算低频区三维雷达目标RCS,与实验数据比较取得良好的计算结果,对RCS理论计算的工程应用起重要作用. 相似文献
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提出了一种求解材料表面不连续目标的散射场的计算方法.这种表面不连续结构是由同厚度的金属半平板和介质半平板相互连接而形成.解决问题的基本思想是把总的散射场分成几个部分,包括直接散射、由平面波对末端开口的平行板波导入射所产生的耦合场以及它们的绕射和反射问题,并分别考虑其对总散射场的贡献.利用此结果,对飞行器座舱的金属-介质连接结构进行了计算,最终结果和文献结果符合的较好. 相似文献
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F. Sabri N. Leventis J. Hoskins A.C. Schuerger M. Sinden-Redding D. Britt R.A. Duran 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2011
Room temperature vulcanizing (RTV)-based components have been used on Mars Pathfinder, the Mars rovers, Spirit and Opportunity, as well as the Phoenix Lander as a support matrix for pigmented panoramic camera calibration targets. RTV 655 has demonstrated superiority to other polymers due to its unique range of material properties namely mechanical stability between −115 and 204 °C and UV radiation tolerance. As a result, it has been the number one choice for many space-related missions. However, due to the high mass density and the natural tendency for electrostatic charging RTV materials have caused complications by attracting and retaining dust particles (Sabri et al., 2008). In the current project we have investigated the relevant properties of polymer-reinforced (crosslinked) silica aerogels with the objective of substituting RTV-based calibration targets with an aerogel based design. The lightweight, mechanical strength, ability to accept color pigments, and extremely low dust capture makes polyurea crosslinked aerogels a strong candidate as a chromatic standard for extraterrestrial missions. For this purpose, the reflection spectra, gravimetric analysis, and low temperature response of metal oxide pigmented, polyurea crosslinked silica aerogels have been investigated and reported here. 相似文献
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Swirl recovery vanes(SRVs) are a set of stationary vanes located downstream from a propeller, which may recover some of the residual swirl from the propeller, hoping for an improvement in both thrust and efficiency. The SRV concept design for a scaled version representing the Fokker 29 propeller is performed in this paper, which may give rise to a promotion in propulsive performance of this traditional propeller. Firstly the numerical strategy is validated from two aspects of global quantities and the local flow field of the propeller compared with experimental data, and then the exit flow together with the development of propeller wake is analyzed in detail.Three kinds of SRV are designed with multiple circular airfoils. The numerical results show that the swirl behind the propeller is recovered significantly with Model V3, which is characterized by the highest solidity along spanwise, for various working conditions, and the combination of rotor and vane produced 5.76% extra thrust at the design point. However, a lower efficiency is observed asking for a better vane design and the choice of a working point. The vane position is studied which shows that there is an optimum range for higher thrust and efficiency. 相似文献
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宫峰勋 《中国民航学院学报》2001,19(6):45-46,52
根据雷达目标测绘区域的特点,结合地面目标的特性系统,给出了合成孔径雷达的目标测绘区域目标的模拟目标模型。根据该区域目标模型可以计算出测绘区域的目标回波信号,经处理后得到测绘区域图像。实验结果表明该区域目标模型可满足对目标回波的处理要求。 相似文献
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一种深空探测器自主天文导航新方法及其可观测性分析 总被引:1,自引:1,他引:1
天文导航是一种适用于深空探测器的完全自主的导航方法,与传统的直接利用天体观测信息进行滤波的方法不同,针对深空探测器,提出了一种首先利用天文观测信息通过几何解算得到一个初步的定位结果,再结合轨道动力学方程利用多模自适应(MM)滤波方法对初步结果进行再处理的自主天文导航新方法,仿真计算的结果表明,该方法可以明显提高导航定位精度,同时从可观测性和可观测度的角度,分析了应用该方法提高导航定位精度的原因和机理。 相似文献