共查询到20条相似文献,搜索用时 46 毫秒
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Tae-Wuk Bae Byoung-Ik Kim Young-Choon Kim Sang-Ho Ahn 《Infrared Physics & Technology》2012,55(5):431-441
In directed infrared countermeasures (DIRCM), the purpose of jamming toward missiles is making missiles miss the target (aircraft of our forces) in the field of view. Since the DIRCM system directly emits the pulsing flashes of infrared (IR) energy to missiles, it is more effective than present flare method emitting IR source to omni-direction. In this paper, we implemented a reticle seeker simulation tool using MATLAB-SIMULINK, in order to analyze jamming effect of spin-scan and con-scan reticle missile seeker used widely in the world, though it was developed early. Because the jammer signal has influence on the missile guidance system using its variable frequency, it is very important technique among military defense systems protecting our forces from missiles of enemy. Simulation results show that jamming effect is greatly influenced according to frequency, phase and intensity of jammer signal. Especially, jammer frequency has the largest influence on jamming effect. Through our reticle seeker simulation tool, we can confirm that jamming effect toward missiles is significantly increased when jammer frequency is similar to reticle frequency. Finally, we evaluated jamming effect according to jammer frequencies, by using correlation coefficient as an evaluation criterion of jamming performance in two reticle missile seekers. 相似文献
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Richard Peter Birchenall Mark A. Richardson Brian Butters Roy Walmsley 《Infrared Physics & Technology》2011,54(5):412-421
The paper describes the concept of missile evolution and the development of a range of missile advancements designed to defeat the evolving array of aircraft defensive measures. The paper describes a typical military aircraft infrared signature and looks at how examination of different spectral parts of the target signature can be used to determine if an aircraft has deployed flare countermeasures. This information can then be used to trigger a missile countermeasure in attempt for the missile to continue with a successful engagement. The paper examines the Track Angle Bias missile countermeasure and details the results of over 1000 engagement simulations designed to test the effectiveness of the missile countermeasure. The paper references the work published in IRPT Volume 53, Issue 5, September 2010, Pages 372–380. 相似文献
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Richard P. Birchenall Mark A. Richardson Butters Brian Walmsley Roy 《Infrared Physics & Technology》2010,53(5):372-380
The global proliferation of shoulder launched IR Man Portable Air Defence Systems (ManPADS) has resulted in the existence of a serious threat to both civilian and military aircraft from terrorist attack. Some of the older generations of ManPADS can be defeated with modern countermeasures but even the most sophisticated protection still has vulnerabilities to the latest family of ManPADS. This paper describes the work undertaken by the authors to model a second generation ManPAD, based on the Russian SA-14, and assess the vulnerabilities of aircraft both with and without flare countermeasures from these systems. The conclusions are the results of over 11,000 simulated firings against targets of varying aspects, velocities and altitudes. 相似文献
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共形整流罩像差特性分析及校正方法 总被引:3,自引:1,他引:2
共形结构不仅具有良好的空气动力学性能,且不存在由于表面不连续造成的热梯度等问题,因而采用该结构的导弹整流罩更有利于导弹系统作战性能的提高。但共形结构中采用的非球面罩曲面使整流罩表现出许多不同于球形结构的动态特性,这给导引头中光学系统的设计带来很多困难。在分析共形结构一阶特性的基础上,利用矢量像差理论详细分析该结构中初级像差产生的原因及特点,并提出通过控制元件的倾斜和偏心来平衡所有观察视场中像差的方法。软件分析结果表明:加入倾斜偏心元件后可适当放大小观察视场中的像差,共形整流罩在各观察视场中具有较为稳定的像差特性,有效地改善了该结构的成像质量。 相似文献
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为消除温度变化对共形光学导引头像质的影响,利用光学被动消热差理论对具体设计方法进行实际分析.根据消热差条件选择合理的透镜材料组合,利用衍射元件特殊的光热特性采用折/衍混合结构进行消热差设计.采用椭球形共形整流罩结构减小空气阻力,降低导弹头部气动加热效应,利用三片式反远距结构实现短焦大视场系统设计.该系统工作波段为3~5 μm,系统F/#为2,视场角为±90°;凝视结构的导引头光学系统后工作距达22.8 mm,为制冷型探测器留有足够的空间;冷光阑效率为100%;在-40℃~60℃温度变化范围内,15 lp/mm处全视场MTF值均大于0.4,满足高准确度定位导引头系统对成像质量的要求,保证了系统的轻小型设计. 相似文献
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超大视场红外告警系统的成像特点分析 总被引:1,自引:0,他引:1
为了设计出适用于超大视场红外鱼眼告警系统的有效算法,对超大视场红外鱼眼告警系统所拍摄的红外图像进行分析,结果发现:超大视场红外图像中目标只表现为一个点,红外图像的背景非常复杂;对于天空背景,随着仰角的增大,其辐射亮度逐渐变小,目标的运动轨迹被弯曲,并随视场角的增大其弯曲程度越甚。从红外鱼眼镜头的设计理论出发,对系统的像面照度进行了分析,并采用美国光电工业公司的CDS100-04型黑体作为标准辐射源对分析结果进行了实验验证,结果表明:不同位置处灰度值的相对标准偏差仅为2.26%,说明该系统的像面照度是均匀的;最后,对系统的作用距离进行了分析,其作用距离约为9.6 km,基本满足实际需要。 相似文献
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针对半实物仿真中定向红外对抗系统的有效模拟问题,在分析定向红外对抗激光源技术的基础上,依据实战应用,计算得到3 m~5 m波段定向红外对抗激光源的辐射能量为飞机红外辐射强度绝对值的8倍,结合波长4 m处简化的大气传输透过率随传输距离的变化,推导出实战应用中红外导引头上辐射照度随飞机导弹之间距离的变化规律。设计半实物仿真中定向红外对抗的模拟方案,依据逼真模拟的原则,计算得到模拟激光源能量随飞机导弹之间距离和飞机辐射强度的变化规律,据此将飞机导弹相互距离1 km时刻的红外干扰源辐射能量设置为波长4 m模拟激光源能量,其他距离的模拟能量通过衰减片来控制。为提高定向红外对抗模拟的通用性和智能性,设计了模拟激光源的闭环控制方案。 相似文献
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主要研究导弹高超声速飞行时弹头流场对自身红外导引头的辐射照度影响问题.建立导弹弹头及气动流场模型,划分计算流场网格、红外导引头镜面网格和辐射场计算网格.从辐射照度和亮度的理论公式开始,推导出适用于辐射网格的气体辐射积分式,并将流场网格数值插值到辐射场网格,求出各节点辐射值得到由导弹飞行状态确定的导弹头部流场气体辐射,积分到红外导引头的光学系统镜面处,求出对其红外导引头的光学系统镜面处的辐射照度.得出流场气体对导引头主镜面的辐射照度值的分布规律:主镜面中心最大,围绕主镜面中心成环形分布,沿着半径方向逐渐减小,随着Mach数增大影响增加. 相似文献
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The Periodically Rotated Overlapping ParallEL Lines with Enhanced Reconstruction (PROPELLER) method for magnetic resonance imaging data acquisition and reconstruction has the highly desirable property of being able to correct for motion during the scan, making it especially useful for imaging pediatric or uncooperative patients and diffusion imaging. This method nominally supports a circular field of view (FOV), but tailoring the FOV for noncircular shapes results in more efficient, shorter scans. This article presents new algorithms for tailoring PROPELLER acquisitions to the desired FOV shape and size that are flexible and precise. The FOV design also allows for rotational motion which provides better motion correction and reduced aliasing artifacts. Some possible FOV shapes demonstrated are ellipses, ovals and rectangles, and any convex, pi-symmetric shape can be designed. Standard PROPELLER reconstruction is used with minor modifications, and results with simulated motion presented confirm the effectiveness of the motion correction with these modified FOV shapes. These new acquisition design algorithms are simple and fast enough to be computed for each individual scan. Also presented are algorithms for further scan time reductions in PROPELLER echo-planar imaging (EPI) acquisitions by varying the sample spacing in two directions within each blade. 相似文献
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对于采用复合制导的空地导弹,中末制导交接班问题是影响命中概率的关键因素。针对这一问题,采用变结构理论设计中制导律。首先建立滑模面,保证滑模面上速度矢量与视线重合,且零化视线角速率,然后设计到达函数,使到达条件得到满足,可以保证交班时刻导弹可靠捕获目标,并为末制导提供最优初始条件。建立了导弹六自由度数学模型和目标捕获模型,进行全系统数字仿真,实验结果表明:在中末制导交接时刻,弹目视线与导弹速度矢量基本重合,误差为0.12°,视线角速度为-0.02°/s,在±20°视场下满足捕获需求,并且为末制导提供最优初始条件。该方法可以满足中末制导交接班要求,具有较强鲁棒性,且中制导段弹道平滑,需用过载小。 相似文献
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Hermann Kick Volker Tank Erwin Lindermeir 《Journal of Quantitative Spectroscopy & Radiative Transfer》2005,92(4):447-455
The impact of changes of the spectral radiance in a Fourier transform spectrometer's field of view (FOV) during recording time of an interferogram is examined. Particularly systematic changes, with a time constant which is in the order of the time required to record one interferogram, are of interest here. Both an analytic and a simulative approach is made to examine the impact on the measured spectrum. Airborne measurements of fire scenes are a typical example where changes of spectral radiance during data acquisition time are inevitable. In such cases, flight velocity causes the scene in the spectrometer's FOV to change continuously, and the scene elements (fire, for example) might be expected to be dynamical even by themselves. 相似文献
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针对综合电子战防区外空地电视遥控指令制导导弹武器系统,建立了载机空间运动、导弹制导飞行、目标的探测与识别和地面有源干扰站、云层、烟幕对空地电视遥控指令制导导弹的干扰模型和作战效能评估模型;对空地电视遥控指令制导导弹武器系统精度和效能进行了仿真分析。结果可用于空地电视遥控指令制导导弹武器系统的精度分析和性能评估,对电视遥控制导导弹的设计研制和作战使用都具有重要意义。 相似文献
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《Radiation measurements》2001,34(1-6):193-197
A spectrometer of the linear energy transfer (LET) based on the chemically etched polyallyldiglycolcarbonate (PADC) track etched detector was developed. The LET spectra are determined through the measurements of track parameters, it covers LET range between 10 and 700 keV/μm in tissue. A combined experimental and theoretical approach allowed the estimation of the critical dimensions of the sensitive volume necessary for developing a track to several nm. It seemed interesting to us to compare the LET spectra obtained by this method with the microdosimetric spectra available on the basis of a classical experimental microdosimetry method, a tissue equivalent proportional counter, for which the critical dimensions simulated are of the order of a few μm.
Both methods of experimental microdosimetry were compared in the high energy radiation reference fields and on the subsonic aircraft board. It was found out that the microdosimetric distributions are similar; some differences are, nevertheless, observed. Further studies with the goal to explain them are outlined. 相似文献