分数维方法研究Alx Ga1-x As衬底上GaAs薄膜中极化子特性随Al浓度的变化

用分数维方法研究AlxGa1-x As衬底上GaAs薄膜中的极化子,得到了衬底中Al摩尔分数x对GaAs薄膜中极化子的结合能和有效质量的影响,极化子的结合能和有效质量的相对变化(mass shift)都随着Al摩尔分数的增大而单调增大;AlxGa1-x As衬底中Al摩尔分数对不同厚度的GaAs薄膜中极化子的影响程度不同,GaAs薄膜的厚度越小,衬底中Al摩尔分数对GaAs薄膜中极化子的影响越显著.     

Multi-dimensional scattering properties diagnosis system of scale aircraft model in an anechoic chamber

Aiming at the concept of ＂diagnosis＂, a simple and effective broadband radar cross section （RCS） measurement system is constructed, and some multi-dimensional scattering properties diagnosis techniques are presented based on the system. Firstly, a stepped-frequency signal is employed to achieve high range resolution, combining with a variety of signal processing tech- niques. Secondly, cross-range resolution is gained with a rotating table, and the high-resolution two-dimensional （2-D） imaging of the scale model is obtained by the microwave imaging theory. Finally, two receiving antennas with a small distance in altitude are used, and the three-dimensional （3-D） height distribution of scattering points on the scale model is extracted from the phase of images. Some typical bodies and a scale aircraft model are diagnosed in an anechoic chamber. The experimental results show that, after scaling with a metal sphere, the accurate one- dimensional （l-D） RCS pattern of the model is obtained, and it has a large dynamic range. When the bandwidth of the transmitting signal is 4 GHz, the resolution of the 2-D image can reach to 0.037 5 m. The 3-D height distribution of scattering points is given by interferometric measurement. This paper provides a feasible way to obtain high-precision scattering properties parameters of the scale aircraft model in a conventional rectangular anechoic chamber.     

基于IRLS的跳频模式下GTD散射参数提取和RCS重构

现代谱估计方法能够反演基于几何绕射理论(geometric theory of diffraction, GTD)的模型参数，但不能处理非均匀不完备的雷达散射截面(radar cross section, RCS)数据。此外，通过暗室测量获取完备的RCS数据也需要较大的时空开销。针对上述问题，提出一种基于迭代加权最小二乘(iteratively reweighed least squares, IRLS)的跳频模式下GTD散射参数提取和RCS重构方法。该方法将稀疏重构理论与GTD散射模型相结合，能够在RCS数据非均匀不完备的条件下反演散射参数和实现RCS重构。仿真数据和电磁计算数据用于验证所提方法的有效性，实验结果表明该方法对降低暗室步进频率RCS的测量成本和扩增雷达RCS数据具有重要意义。     

采用自适应原始对偶迭代的无人机编队协同航路规划方法

针对目标通过机动进入无人机雷达探测盲区、导致雷达跟踪不稳定的问题，提出一种无人机编队协同航路规划方法。首先，根据雷达多普勒速度盲区、雷达探测视角、距离边界区等建立协同航路规划约束条件；然后，以机动目标稳健跟踪为目的建立优化目标函数，并结合约束条件构建协同航路优化模型；最后，设计了一种自适应原始-对偶迭代算法，对建立的航路优化模型进行快速求解，得到无人机飞行实时航路。对比仿真结果表明：所提方法能够实现无人机编队协同航路快速规划，达到对机动目标持续稳定跟踪的目的；与传统的高斯伪谱法和模型预测控制算法相比，所提方法求解速度提升了10%,算法复杂度相对较低；所提方法求解的无人机航路平滑性较好，可减少无人机飞行油耗，便于长时留空探测。     

分布式MIMO体制天波超视距雷达仿真系统

针对电离层动态性对天波超视距雷达检测概率和探测精度的影响，构建了一种基于分布式多输入多输出(multiple input multiple output, MIMO)体制的完整天波超视距雷达仿真系统。通过搭建模块化仿真框架和可视化展示界面，集成电离层数据接口，实现信号发射、电离层反射、信号接收、信号处理和目标检测的功能。最后对雷达系统探测性能进行评估，利用仿真实例验证了整体雷达仿真系统的可行性。该系统的实现对于分布式MIMO天波超视距雷达的性能评估、布站优化、装备发展论证具有一定的工程指导意义。     

雷达角误差信号的数字化算法

阐述了一种数字化的雷达单脉冲系统,在比幅体制的单脉冲天线下,提出了相应的角误差计算方法,并给出了一种工程中实际使用的方法,总结了该方法的使用效果。     

Atmospheric duct estimation from multi-source radar sea clutter returns: theoretical framework and preliminary numerical results

Refractivity from clutter （RFC） technique estimates lower atmospheric refractivity from radar sea clutter returns. An important issue of RFC is how to make the estimate more robust. Rather than using only single beam radar sea clutter returns, this paper puts forward a theoretical framework of combining multi-source clutter power to improve the retrieved results by the variational adjoint approach. The derivation of the adjoint is accomplished by an analytical transformation of the parabolic equation model in a continuous domain. To test the theoretical algorithm, numerical simulations using multi-elevation clutter observations are carried. The results demonstrate that combining two elevation beams gives more stable estimate than using only single beam.     

一种VTS雷达中心机的设计与实现

本文根据VTS雷达的系统设计需求,给出了一种中心机设计方案,介绍了外部接口设计和硬件选取方案,对软件的总体结构和主要流程等进行了设计,并对其中的一些关键技术进行了论述。     

Ion flux dropout observed near dipolarization front

An ion flux dropout near the dipolarization front （DF） at around XGSM =- 11 RE in the Earth＇ s plasma sheet was observed by Time History of Events and Macroscale Interaction during substorms （THEMIS） on March 31, 2009. The ion differential energy fluxes at energies from 450 eV to 150 keV measured by the ESA and SST instruments from THC began to decrease about 2 s before the detection of the DF and reached a local minimum 6 s later. Then, the ion fluxes gradually increased to form a dropout around the DF. The spatial extent of the dropout was about 4,000 km. For energies above 20 keV, the ion fluxes after the dropout are greater than those before it, contrary to the fluxes at energies below 20 keV. The associated ion density variation indicates that the ion flux dropout coincides with the ion density dropout. Taking advantage of multipoint observations, THD, THC, and THE detected the same DF consecutively. Only THC detected an obvious ion flux dropout; THD observed an indistinct one about 2 s before THC; no high-energy （E 〉 30 keV） ion flux dropout was observed by THE. Our study suggests that the ion flux dropout may evolve with the earthward-propagating DF, and its properties can depend on locations relative to the DF.     

组网雷达探测能力的并行计算与可视化方法研究

深入研究了并行计算与并行绘制相结合的并行框架构建问题。针对组网雷达探测能力的计算与可视化特点,在(PC)集群的基础上,构建了一个并行计算与可视化运行框架。该框架在并行计算中,采用八叉树分割的方法对组网雷达计算区域进行任务分配；在并行绘制中,采用sort-last的并行绘制机制。仿真试验结果表明,该运行框架能够有效地满足大规模组网雷达探测能力计算与可视化的应用需要。