星载SAR椭圆轨道全零多普勒导引方法研究

多普勒中心频率在星载合成孔径雷达（SAR）成像中,直接影响方位向的模糊度及图像的定位精度。全零多普勒导引方法通过调整偏航角和俯仰角,使多普勒中心频率为零,但现有方法都导致残余多普勒中心频率较大。文章利用椭圆轨道下多普勒中心频率的表达式,将多普勒中心频率分为仅与俯仰角相关部分,以及与俯仰角和偏航角都相关的部分,令两部分分...     

苏/俄交会对接技术研究

苏/俄交会对接技术的研发,最初是为20世纪60年代初苏联月球使命服务的,后来主要用于空间站的运输使命。因此,最初的＂联盟＂飞船逐步演变发展为联盟号载人飞船系列与进步号货运飞船系列。联盟号和进步号飞船应用＂指针＂或＂航向＂交会雷达系统,基本采用自动轨道交会方法。对应急运作,联盟号航天员可使用手控器;对于不载人的进步号使命...     

基于模糊数学的民机机载气象雷达故障诊断

将模糊数学方法引入到民机机载气象雷达故障诊断中．提出由历史数据及专家择优综合确定模糊隶属度的方法,建立了模糊故障诊断模型,准确、快速地找出故障原因,实践证明该模型合理有效。     

TOPSAR data focusing based on azimuth scaling preprocessing

Both Doppler spectral aliasing and azimuth output time folding simultaneously exist in TOPSAR (Terrain Observation by Progressive Scans) raw data. Resampling in both Doppler frequency and azimuth time domain can resolve the azimuth aliasing problem but with the seriously increased computational complexity and memory consumption. According to the special characteristics of TOPSAR raw data support in the slow time/frequency domain (TFD), the presented azimuth scaling preprocessing step is introduced to not only resolve the Doppler spectral aliasing problem but also reduce the increased azimuth samples. Furthermore, the correction of sawtoothed azimuth antenna pattern (AAP) becomes easy to be implemented. The following conventional stripmap processor can be adopted to focus the residual TOPSAR raw data but with the result of azimuth aliased TOPSAR image. The mosaic approach, which has been presented to unfold azimuth aliased ScanSAR image, is exploited to resolve the problem of azimuth output folding in TOPSAR mode. Simulation results and pulse response parameters are given to validate the presented imaging approach.     

The possibilities of polar meteorology,environmental remote sensing,communications and space weather applications from Artificial Lagrange Orbit

The ability to observe meteorological events in the polar regions of the Earth from satellite celebrated an anniversary, with the launch of TIROS-I in a pseudo-polar orbit on 1 April 1960. Yet, after 50 years, polar orbiting satellites are still the best view of the polar regions of the Earth. The luxuries of geostationary satellite orbit including rapid scan operations, feature tracking, and atmospheric motion vectors (or cloud drift winds), are enjoyed only by the middle and tropical latitudes or perhaps only cover the deep polar regions in the case of satellite derived winds from polar orbit. The prospect of a solar sailing satellite system in an Artificial Lagrange Orbit (ALO, also known as “pole sitters”) offers the opportunity for polar environmental remote sensing, communications, forecasting and space weather monitoring. While there are other orbital possibilities to achieve this goal, an ALO satellite system offers one of the best analogs to the geostationary satellite system for routine polar latitude observations.     

基于时频原子方法的雷达辐射源个体识别

针对雷达辐射源个体识别问题,提出一种时频原子分解的特征提取方法.该方法针对主振放大式发射机,首先根据锁相环频率合成器相位噪声的功率谱,模拟含有特定相位噪声的辐射源信号.然后基于时频原子分解原理并采用膜算法将带有相位噪声的辐射源信号在正弦原子库中进行一次分解.最后利用分解后的原子提取出正弦原子能量特征和原子频率偏差特征,...     

连续波雷达信号的侦收与处理

叙述分析处理连续波（ＣＷ）信号的重要性，并介绍测定ＣＷ信号频率特征的方法。讨论了运行载体上的ＣＷ信号频率的调制特性和多普勒频移以及侦收系统噪声对测定信号频率的影响。     

基于雷达散射截面约束的气动优化设计

采用拉格朗日乘子法优化设计了雷达散射截面约束条件下的锥形融合气动外形.拉格朗日乘子法中的极小化问题采用动态演化的优化设计方法求解.该方法是一种基于非定常演化的优化设计方法,即在求解非定常流动支配方程的时候同时履行优化过程,较其它基于定常解的优化方法具有高得多的计算效率.其中的雷达散射截面通过求解非结构的笛卡儿网格上的时域麦克斯韦方程来得到,而升阻比则通过求解锥形流方程来计算.通过优化设计,得到了M∞=8.0时,升阻比为4.98,雷达散射截面只有1.66m2的锥形融合气动外形.     

Lower ionosphere response to external forcing: A brief review

There are two ways of external forcing of the lower ionosphere, the region below an altitude of about 100 km: (1) From above, which is directly or indirectly of solar origin. (2) From below, which is directly or indirectly of atmospheric origin. The external forcing of solar origin consists of two general factors – solar ionizing radiation variability and space weather. The solar ionization variability consist mainly from the 11-year solar cycle, the 27-day solar rotation and solar flares, strong flares being very important phenomenon in the daytime lower ionosphere due to the enormous increase of the solar X-ray flux resulting in temporal terminating of MF and partly LF and HF radio wave propagation due to heavy absorption of radio waves. Monitoring of the sudden ionospheric disturbances (SIDs – effects of solar flares in the lower ionosphere) served in the past as an important tool of monitoring the solar activity and its impacts on the ionosphere. Space weather effects on the lower ionosphere consist of many different but often inter-related phenomena, which govern the lower ionosphere variability at high latitudes, particularly at night. The most important space weather phenomenon for the lower ionosphere is strong geomagnetic storms, which affect substantially both the high- and mid-latitude lower ionosphere. As for forcing from below, it is caused mainly by waves in the neutral atmosphere, i.e. planetary, tidal, gravity and infrasonic waves. The most important and most studied waves are planetary and gravity waves. Another channel of the troposphere coupling to the lower ionosphere is through lightning-related processes leading to sprites, blue jets etc. and their ionospheric counterparts. These phenomena occur on very short time scales. The external forcing of the lower ionosphere has observationally been studied using predominantly ground-based methods exploiting in various ways the radio wave propagation, and by sporadic rocket soundings. All the above phenomena are briefly mentioned and some of them are treated in more detail.     

腹部进气道电磁散射特性及RCS减缩方法研究

对建立的腹部S型进气道及前机身模型,采用多层快速多级子方法计算雷达散射截面,研究了进气道唇口斜切方式、上下唇边锯齿化、S型弯道长度、等直段安装吸波导流环和前机身形状对腹部进气道头向RCS的影响,并分析进气道与前机身的耦合散射特性。通过计算进气道参数改变前后的电磁散射特性,找出影响腹部进气道头向雷达散射截面的主要因素和RCS减缩方法,并对各种减缩方法的减缩效果作了对比分析。研究结果为腹部进气道的头向RCS减缩提供了技术依据。