一种多路通用基带处理硬件平台设计

介绍一种应用于各种信号体制的多路通用基带处理硬件平台的设计方案,并详细说明硬件平台的组成及性能。平台采用LVDS串行技术,大大提高了硬件集成度;同时采用低抖动时钟方案和LVPECL差分时钟,使得硬件平台的整体性能大幅度提升。最终,在较小面积的印制板上实现了16路数字接收通道,并包含了当前主流中央处理器DSP、两片大容量FPGA以及大容量外部存储器FLASH。方案可适用于处理较多输入信号的情况。     

基于第二代小波包解调技术的船载天线轴承故障诊断方法研究

针对船载天线传动机构中滚动轴承易损坏问题,研究基于第二代小波包解调技术的轴承故障诊断方法。首先将原始振动信号进行第二代小波包分解和分频带重构,求得各频带重构信号的希尔伯特包络谱分贝值;然后分别提取各频带包络谱中轴承故障特征频率处的分贝值,从而得到最大分贝值;最后依据冲击脉冲法故障等级经验计算公式识别轴承的状态。实际应用结果表明,第二代小波包解调技术可实现轴承故障的定位定量诊断。     

EHF频段低噪声放大器设计

EHF频段低噪声放大器是EHF频段接收机系统的关键部件。文章介绍了利用混合集成技术设计的43.5GHz～44.5GHz的低噪声放大器。该低噪放采用BJ400标准矩形波导作为输入输出端口,通过鳍线耦合实现了微带到波导的过渡,采用一种新型电路构型实现电路设计。从测试结果可以看出,采用对脊鳍线过渡方式的EHF频段低噪声放大器中心频率偏移到43GHz,在常温状况下,在42.7GHz～43.2GHz带宽内增益为19dB左右,噪声系数小于5dB。     

Ionospheric disturbances on 8 September, 2010: Was it connected with the incoming moderate Chongqing earthquake?

Earthquake prediction stimulates the searches for a correlation between seismic activity and ionospheric anomalies. Contrary to common focuses on strong earthquakes, we report the ionospheric disturbances, 2 days before a moderate Ms = 4.7 Chongqing earthquake (29.4°N, 105.5°E, depth = 7.0 km, occurred at 21:21 LT, 10 September, 2010) with the data of ground-based ionosondes and IGS receivers. The data covering the period under the quiet geomagnetic conditions and a geomagnetic storm was analyzed with upper and lower bounds. It is found that there were significant enhancements of foF2 and total electron content (TEC) on the afternoon of 8 September, 2010, with a limited area close to the epicentre, which was different from the feature of ionospheric perturbations triggered by the geomagnetic storm on 15 September. Taking into account the heliogeomagnetical condition, we conclude that the observed ionospheric enhancements were very likely associated with the forthcoming moderate Chongqing earthquake, which implies that the relationship between the amplitudes of ionospheric disturbances and earthquakes is very complicated.     

月面重力模拟系统恒拉力绳索的动力学研究

月面巡视器在未来探月工程中有非常重要的作用.月球重力场是影响月面巡视器运动性能的重要环境因素,需要对其进行地面模拟试验.文章基于绳索悬挂建立月面重力模拟系统,其关键是对恒拉力绳索进行建模和动力学分析.通过将绳索离散化为一系列集中质量的弹簧阻尼结构,得到多刚体系统来代替连续的弹性系统,用数值计算方法来研究绳索系统的动力学参数(如刚度和阻尼)对月面重力模拟系统的影响,来优化月面重力模拟系统.     

激光外差干涉技术在固体发动机振动中的应用

利用激光外差干涉技术对工作中固体火箭发动机的振动频率及强度进行了研究。在实验室环境下建立一套激光外差干涉系统,对某型号发动机进行振动测量实验。实验表明,激光外差干涉测振系统测量带宽7.8 Hz,测量标准偏差小于5.6×10-8,振镜实验测量结果与振源频率相吻合,系统探测信号强度和物体振幅呈线性关系。激光外差干涉技术在发动机振动测量过程中具有一定的应用价值。     

退火温度对Al-Mg 合金拉伸性能和显微组织的影响

通过硬度、拉伸性能测试和金相组织观察,研究了不同退火温度对含和不合Sc的Al-Mg合金组织和性能的影响.结果表明:添加Sc明显提高了Al-Mg合金的强度,抑制了合金形变组织的再结晶,高温退火后1570合金中仍弥散分布的Al3( Sc,Zr)粒子质点造成其较高的再结晶温度及拉伸性能.     

Suborbital and low-thermospheric experiments using sounding rockets in Taiwan

The suborbital flight is a kind of flight, which reaches the space and then comes back to ground without completing one orbital revolution. The atmospheric thermosphere extends from 85 km to 600 km in altitude. Therefore, the suborbital and low-thermospheric experiments to be performed at altitude below 300 km can be combined using the sounding rocket. These experiments include rocket staging, fairing separation, ultrasonic flight, reentry, aerobrake and recovery test, ultraviolet and ionization observations, ozone measurement, etc. The advent of Taiwan's sub-orbital and thermospheric experiments project can be traced back to 1997. This is the year Taiwan's National Space Organization (NSPO) was assigned to be responsible for procuring the sounding rocket for applications in science experiments and space technology research effort. From 1997 to 2010, 8 launches have been completed including one experimental hybrid rocket. All onboard instruments and sensors for sub-orbital and low-thermospheric experiments are developed and integrated by the domestic universities. More launches have been planned in the future. Opportunities for international cooperation in developing new instruments and payloads for future experiments will be possible.     

基于稀疏重构的L型阵列的二维波达方向估计

在L型阵列下,基于稀疏重构提出一种可实现自动角度配对的二维波达方向估计方法。首先,根据两均匀线阵接收数据的互相关矩阵构建二维稀疏线性模型;然后,通过数学变换将该二维模型转换为联合稀疏重构模型之内,通过联合稀疏重构算法分别单独获得信源方位角和俯仰角的粗略估计,并将此信息融入二维稀疏线性模型,大大减少了模型中原子个数,达到降低计算复杂度的目的;其次,从理论上分析了新方法可分辨的信源个数和计算复杂度;最后,通过一系列计算机仿真将新方法与其它子空间类二维波达方位估计方法进行比较,表明了新方法在估计精度上的优越性。     

基于协同决策的多航站楼停机位实时分配算法

针对多航站楼机场停机位实时指派问题,提出了基于协同决策并考虑航空公司时隙交换公平性的机位实时指派算法。该算法将多航站楼资源的可共享性考虑到指派算法中,以最小延误费用原则为约束,采用混合集合规划进行指派模型的建立与求解。该算法在保证多航站楼停机位资源有效共享的前提下,充分实现了航空公司时隙交换的公平性,并且使延误引起的多方成本最小化。算例说明:本文提出的算法可以有效解决多航站楼的机位实时分配问题。