共查询到20条相似文献,搜索用时 515 毫秒
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在分析对比现有的雷达罩设计方法基础上,针对某型直升机机栽雷达罩,研究了雷达罩设计过程中的基本问题、关键技术和综合优化设计方法,运用三维射线追踪法进行了计算机辅助设计,给出了布设防雷击部件的经验公式,讨论了吸波材料选择与喷涂的基本准则。电测结果表明:加罩后的功率传输系数、反射瓣、雷达辐射特性等指标的实测数据与计算值符合较好,满足了设计要求。 相似文献
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雷达罩应用5258树脂基复合材料的试验研究 总被引:1,自引:0,他引:1
通过试验研究了雷达罩所用主要材料5258环氧树脂、预浸料和复合材料制备方法,进行了这些材料及结构的拉伸、弯曲、剪切和介电常数等性能的测试,结果表明5258树脂基体制备的复合材料均具有良好的力学和电学性能,能够满足雷达罩的设计要求。 相似文献
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针对某型飞机大修期间经常发现的雷达罩大面积脱胶损伤故障,通过选择修理材料和修理方案,制定了合理的故障修理方案,并通过力学性能试验和电性能对比试验对雷达罩功能恢复情况进行了验证,为飞机雷达罩脱胶故障的排除提供参考。 相似文献
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机载雷达罩技术的发展 总被引:1,自引:1,他引:0
随着机载雷达性能水平的提高,对雷达罩电性能提出了越来越高的要求。本文从电性能的角度介绍雷达罩设计、材料、工艺、质量保证和测试等方面的技术发展情况。 相似文献
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概要介绍了在米格-21飞机新型脉冲多普勒雷达罩电性能设计中进行的技术分析和制定的总体方案,着重介绍以最小功率反射为目标的雷达罩变壁厚设计技术以及该雷达罩通过地面测试及空中飞行试验验证所取得的优良性能。 相似文献
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分析了涂层封存导弹雷达罩透波率与密封性问题,并结合某导弹的实际情况进行了试验,试验结果表明,控制雷达罩的用胶量,即可满足透波率和密封性的要求。 相似文献
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If modern airborne radar systems are to function properly, the radar antenna radiation patterns must meet certain specifications. Until recently, most radar antennas were designed and tested in a clean antenna environment, i.e., there is no near field scattering from host structures or radome effects. However, these higher order effects are the matter of increasing concern with added performance demands in the ever-increasing jammer and clutter interference environments. We investigated the capabilities and limitations of currently available analysis techniques and computer codes for installed performance of airborne radar antenna systems. Then we developed an extended ray-optical technique that could predict total installed performance of airborne radar antenna systems, i.e., the near field scattering from aircraft structures and radome effects. The new analysis technique utilized a ray-tracing method in both airframe and radome simulation. Thus, it can efficiently predict the total installed performance of large radar antenna systems on an aircraft structure 相似文献
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针对导弹雷达导引头天线罩生产过程中的质量偏差问题,利用六西格玛的改进模式——DMAIC,借助统计软件MINITAB,分析并提出了天线罩的生产过程改进方法。结果表明:天线罩厚度是影响生产质量的关键因素,通过控制生产过程中的压力、温度等直接影响因素,能显著提高天线罩生产的质量水平。 相似文献
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Numerous documents were reviewed to verify radar parameters needed to analyze and present the tester concept described herein. The weather and windshear models defined use the identical criteria established for the Doppler radar in terms of F-factor. The basic concept of the tester is to transmit coherent simulated radar returns in response to the airborne radar's transmission while mounted on a tripod in the far field of the radar when parked on the ramp. The varying amplitude of the received radar pulses are analyzed and put into memory as the tester antenna is illuminated by the scanning main beam and side lobes of the radar's antenna patterns. The tester controls the power of its outputted simulated radar returns in inverse relation to the power of the received radar pulses. These simulated radar returns, outputted into the main beam and/or side lobes of the scanning radar antenna, are interpreted by the radar system as received in the main lobe. The tester transmissions, incorporating microburst, storm and gust front models, previously defined, can thereby test the aircraft radar system performance in various hazard environments. The tester is designed to: verify operational performance of the radar; demonstrate installed radar performance; verify crew reports and minimize radar or LRU's removal for maintenance; test before and after a repair; and verify radome effects on radar performance 相似文献
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基于多级维纳滤波的双基地MIMO雷达多目标定位方法 总被引:1,自引:1,他引:0
为了降低双基地多输入多输出(MIMO)雷达目标定位过程中的计算复杂度,避免进行占主要计算量的协方差矩阵特征值分解或奇异值分解和二维空间谱的峰值搜索,将多级维纳滤波(MSWF)应用于双基地MIMO雷达多目标定位的研究中。利用MSWF的前向递推原理,得到信号子空间;然后利用ESPRIT算法估计发射角(DOD)和接收角(DOA),且DOD和DOA自动配对,实现了多目标交叉定位。分析了本文算法和ESPRIT算法的计算复杂度,并通过仿真实验及性能分析验证本文算法的有效性。理论分析和实验结果表明:本文算法在保证二维方位角估计性能的基础上,显著地降低了计算复杂度,缩短了运算时间,更加符合MIMO雷达信号实时处理的要求。 相似文献
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基于3DT的空时自适应单脉冲参数估计算法 总被引:1,自引:0,他引:1
空时自适应处理(STAP)是机载预警雷达抑制杂波和干扰的一项关键技术,而多普勒三通道联合自适应处理(3DT)是适合工程实现的降维(RD)STAP方法。STAP目标检测后还需进一步估计目标的角度参数,因此将自适应单脉冲(AM)技术引入3DT,提出了一种高精度联合估计目标速度与方位空间角的空时自适应单脉冲算法。理论分析与仿真实验结果表明,当目标多普勒频率偏离检测多普勒单元中心频率时,该算法能同时减少目标多普勒跨越损失和空时导引矢量失配损失,进而提高输出信杂噪比(SCNR),改善目标测角精度。 相似文献
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The feasibility of using the indicated quadrature angle of arrival of a monopulse radar to discriminate a single target from multiple targets, separated in angle within a radar resolution cell, is investigated. The analysis is performed for steady (fixed) and Rayleigh fluctuating targets which cover a broad range of target characteristics. In both cases, the interfering signals due to noise and clutter in the sum and difference monopulse channels are assumed to be independent, zero-mean Gaussian processes. Detection and false alarm probabilities are evaluated analytically and the receiver operating characteristics are obtained for both fixed and fluctuating target cases. It is shown that multiple targets can be discriminated from a single target condition by integrating the indicated monopulse quadrature angle of arrival from several independent pulses. It is also shown that the probability of detecting multiple targets increases as the fluctuation in the target radar cross section decreases, approaching the fixed amplitude case in the limit. 相似文献
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三维雷达罩和天线系统雷达截面的一体化分析 总被引:3,自引:0,他引:3
将入射平面波展开成一系列三维复射线波束场,分析各波束经过多层介质雷达罩的透射与旋转抛物面天线反射后,提出了一种等效复射线源来得到最终散射场的方法。设计了反射与透射的通用自动追踪程序,可进行天线和无线罩一体化的雷达载面(RCS)分析,给出了一个数值计算实例。 相似文献
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This paper studies the radar cross section(RCS) of carrier electronic warfare airplanes.Under the typical naval operations section, the mathematical model of the radar wave’s pitch angle incidence range analysis is established. Based on the CATIA software, considering dynamic deflections of duck wing leading edge flaps, flaperons, horizontal tail, and rudder, as well as aircraft with air-to-air missile, anti-radiation missile, electronic jamming pod, and other weapons, the 3D models of carrier electronic warfare airplanes Model A and Model B with weapons were established. Based on the physical optics method and the equivalent electromagnetic flow method, by the use of the RCSAnsys software, the characteristics of carrier electronic warfare airplanes’ RCS under steady and dynamic flights were simulated under the UHF, X, and S radar bands. This paper researches the detection probability of aircraft by radars under the condition of electronic warfare, and completes the mathematical statistical analysis of the simulation results. The results show that: The Model A of carrier electronic warfare airplane is better than Model B on stealth performance and on discover probability by radar detection effectively. 相似文献
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Airborneradomemayintroducesignificantperformancedegradationtoantennaandradarsystems,evenifdesignedelaborately.Sinceradomeisad... 相似文献