长球的双基地雷达截面积计算分析

雷达截面积（RCS）是目标的一个重要特性参数，在理论上分析计算目标的雷达截面积有着重要的实际意义。基于几何光学能量传播的思想，首先推导了一种长球双基地雷达截面积的计算方法，并以此分析了长球的双基地雷达散射截面积，最后对算法进行了仿真计算，仿真结果表明长球的RCS呈现极强的方向性。     

箔条云形状对干扰效果的影响

主要从箔条云的雷达截面入手，考虑箔条云雷达截面积方向性要求，通过计算不同形状箔条云的雷达截面积，提出理想的箔条云形状；并扼要分析它们对质心干扰效果的影响。     

舰用雷达对抗新技术

雷达对抗（ECM）技术在与雷达反对抗（ECCM）技术角逐中不断得到发展。水面舰艇，雷达反射截面积大，机动性差，易受攻击。本文就几种新的雷达对抗技术应用于水面舰艇的电子防卫作了初步探讨。     

影响海上箔条云RCS的因素分析

通过对点目标、海上低空箔条云雷达截面积的理论计算，推导出影响海上箔条云雷达截面积测量值的因素，对主要因素的影响程度进行了理论计算，提出了合理利用海面多路径的方法。     

影响海上箔条云RCS的因素分析

通过对点目标、海上低空箔条云雷达截面积的理论计算，推导出影响海上箔条云雷达截面积测量值的因素，对主要因素的影响程度进行了理论计算，提出了合理利用海面多路径的方法。     

一种测量雷达截面积的方法

介绍了利用对比法对物体RCS进行测量的方法.其过程是采用已知雷达截面积的金属球作为标校物,通过对比获得被测物体的雷达截面积.     

机载箔条诱饵技术指标的测试方法

本文的机载箔条诱饵是指由机载自卫式箔条投放器投放的箔条所形成的箔条云，其技术指标是指箔条云的雷达截面积、箔条云的形成时间和箔条云的频率特性。本文着重叙述箔条云雷达截面积的测试方法。由于箔条云形成时间短、雷达截面积小，因此以往用于测试舰载和地面发射装置箔条云雷达截面积的方法已不适用。为此，本文提出一种用延迟雷达跟踪波门的新方法测试箔条云的雷达截面积。文中叙述了该方法对飞机的飞行参数，雷达性能和测试设     

雷达图象数据的规格化及解释

校准后的雷达图象通常量化为雷达截面积（ＲＣＳ）。从严格意义上说，这一解释并不正确，会使人对测试目标的散射特性产生误解。为了避免不必要的混淆，建议采用“散射亮度”（其定义见下文）这一术语作为图象域数据的标准标记。     

地面双基地雷达箔条干扰研究

在充分考虑双基地雷达工作特点的条件下，首先根据箔条干扰的性质，分析其雷达截面积，其次建立了双基地条件下箔条云团的雷达截面积模型，通过与现有理论的比较，证明了该模型的合理性。最后，建立了箔条云团干扰回波的模型。     

机载箔条诱饵技术指标的测试方法

本文的机载箔条诱饵是指由机载自卫式箔条投放器投放的箔条所形成的箔条云，其技术指标是指箔条云的雷达截面积、箔条云的形成时间和箔条云的频率特性。本文着重叙述箔条云雷达截面积的测试方法。由于箔条云形成时间短、雷达截面积小，因此以往用于测试舰载和地面箔条发射装置箔条云雷达截面积的方法已不适用。为此，本文提出一种用延迟雷达跟踪波门的新方法测试箔条云的雷达截面积。文中叙述了该方法对飞机的飞行参数、雷达性能和测试设备的要求。     

低频太赫兹准目标雷达散射截面的实验研究

以研究太赫兹雷达散射截面的特性为目的,选用所搭建低频太赫兹雷达测试系统,并借助于标准目标法开展了有关太赫兹雷达粗糙铝盘散射截面的实验研究工作.实验结果表明:在小角度散射中太赫兹雷达散射截面随散射角的增大变化比较明显,在散射角超过5后太赫兹雷达散射截面随散射角的变化趋向缓慢,但当散射角超过12后探测信号的强度已衰减到无法测量,在太赫兹雷达散射截面的测试中没有出现微波雷达散射截面的大小随散射角的变化而剧烈振荡的现象;将测试结果与同尺寸微波、激光雷达散射截面的结果进行了对比,得到结论:在0附近太赫兹雷达散射截面的数值比同尺寸微波雷达散射截面的数值要小两个数量级,但比同尺寸激光雷达散射截面的数值要高一个数量级.     

激光雷达截面在系统设计评价中的应用分析

讨论分析了激光雷达截面在激光测量系统设计评价中的应用.分析了激光雷达截面的物理意义,给出了目标激光雷达截面的计算、测量原理与方法,从激光雷达截面的理论定义出发,推导出普遍适用于各类激光测量系统和各种散射特性目标的基本测量方程,该方程利用激光雷达截面表征目标的激光散射特性.通过典型实例说明了该方程在激光测量系统设计评价中的应用.与其他用于表征目标激光散射特性的指标相比,激光雷达截面更容易通过计算或测量得到,且更适用于复杂散射特性目标,因此,在激光测量系统的设计评价中应采用由目标激光雷达截面表述的激光测量方程.     

Radar cross section measurements

The progress in radar cross section measurements is strongly related to the progress in radar technology. The recent acceleration in radar technology and processing techniques has generated a corresponding acceleration in interest for radar cross section measurements. Historically, early radar cross section measurements were performed to determine the detection range of radar systems, a fundamental objective that still exists. Later measurements, coupled with analytic techniques and computer codes, were performed to extend our understanding of the radar scattering process. At the present time, the availability of broad-band electronics, signal processing techniques, and digital technology results in radar cross section measurement programs which are directed toward exploring the performance of operational waveforms and processing, target discrimination, target detectability in clutter, and radar scattering control. The fundamentals of radar cross section measurements are reviewed. Measurement facilities, including the present research activities on compact range techniques, are then described. Instrumentation radars have benefited from both wide-bandwidth electronics and digital processing capabilities; Fourier transform techniques, in particular, provide both additional information on target scattering, and increase measurement accuracy by isolating the target from radar returns from the measurement facility. The frequency coverage has also extended to include millimeter-wave frequencies. Achievable accuracy is important in any measurement program, and those factors that limit the accuracy of radar cross section measurements are discussed.     

The physical optics radar cross section of an elliptic cone

The physical optics approximation is used to evaluate the backseattering radar cross section of a semi-infinite metallic elliptic cone. The resulting formula can be directly interpreted as a generalization Of the well-known formula for the baekscattering cross section of a circular cone. In addition the bistatic radar cross section of the elliptic cone is calculated.     

On the radar cross section of a dipole

Literature references dealing with the radar cross section of a dipole target contain a possible source of confusion in that two definitions of cross section have been used. To clarify this situation, the radar cross section of a randomly oriented half-wave dipole is considered using both definitions.     

The Contribution of Wedge Scattering to the Radar Cross Section of the Ocean Surface

This letter considers the contribution to the radar cross section of the ocean surface due to scattering from edges for which the local radius of curvature is small compared with the radar wavelength. An analytic expression based on the method of equivalent currents is given for such scattering and is evaluated for several assumed sets of parameters. This contribution is shown to augment the Bragg scattering cross section in regions where the latter underestimates the measured radar cross section, while remaining smaller than the Bragg component elsewhere.     

太赫兹雷达散射截面测量中定标体的确定

围绕赫兹雷达散射截面定标体选定的内容开展了一系列工作,确定了适合作为太赫兹雷达散射截面标准体的工艺要求和加工方式,并先后对6种通过不同工艺加工成的太赫兹雷达散射截面的标准体材料进行了测试,分别测出半球反射率随波长的变化关系,确定了适合作为太赫兹雷达散射截面标准体的工艺要求和加工方式,加工出符合条件的太赫兹雷达散射截面测量中用作定标金属铝球,并利用该定标体对其他目标体在低频太赫兹波段的雷达散射截面进行了初步测量。     

防空雷达飞机目标调制周期特征的研究

基于飞机旋转部件对雷达电磁波调制机理,以及对调制参数模型和回波特点的分析理解,本文针对防空雷达,分析了几种飞机目标的调制周期特征,提出了几种调制周期特征分析和提取的方法.本文的主要贡献是揭示了防空雷达飞机回波复包络中的调制周期特征,分析了在不同飞机姿态、不同雷达工作状态下实际回波中调制周期特征的稳定性,并讨论了调制周期特征用于辨识螺旋桨飞机的可能性.实测数据分析结果表明:本文方法能从防空雷达螺旋桨飞机回波中提取调制周期特征,并用于螺旋桨飞机的辨识.     

The radar cross section of dielectric disks

A solution is presented for the backscatter (monostatic) radar cross section of dielectric disks of arbitrary shape, thickness, and dielectric constant. The result is obtained by employing a Kirchhoff-type approximation to obtain the fields inside the disk. The internal fields induce polarization and conduction currents from which the scattered fields and the radar cross section can be computed. The solution for the radar cross section obtained in this manner will be shown to agree with known results in the special cases of normal incidence, thin disks, and perfect conductivity. It will also be shown that the solution can be written as a product of the reflection coefficient of an identically oriented slab times the physical optics solution for the backscatter cross section of a perfectly conducting disk of the same shape. This result follows directly from the Kirchhoff-type approximation without additional assumptions.     

Radar cross-section study of cylindrical cavity-backed apertureswith outer or inner material coating: the case of E-polarization

A dual-series-based solution is obtained for the scattering of an E-polarized plane wave from a cavity-backed aperture which is formed by a slitted infinite circular cylinder coated with absorbing material. The material coating can be done on the inner or outer surface of the cylinder. For both cases, numerical results are presented for the radar cross section and comparisons are given for two different realistic absorbing materials. The radar cross-section results are also given for the aspect angle of the screen. Finally, the dependence of radar cross section on the thickness of the absorbing layer is presented