套筒天线组成的宽带干涉仪测向圆阵研究

为提高宽带干涉仪测向圆阵性能,首次提出了利用套筒天线代替常规加载宽带偶极子作为测向阵列单元.利用Fourier变换结合矩量法分析了套筒天线组成的测向圆阵的电磁特性,并利用HFSS软件对部分仿真结果进行了验证.在得出阵列电磁特性的基础上再运用基于空间距离的相关数据处理方法统计分析了测向圆阵性能.研究结果表明,相对于常规测向圆阵,由于套筒天线构成的测向圆阵增益高、消除了广义谐振现象,使测向圆阵的灵敏度、测向精度均得到较大提高.相应地模糊度减小、稳健性能增强.     

Mid-latitude thermospheric wind changes during the St. Patrick’s Day storm of 2015 observed by two Fabry-Perot interferometers in China

In this work, we utilize thermospheric wind observations by the Fabry-Perot interferometers (FPI) from the Kelan (KL) station (38.7°N, 111.6°E, Magnetic Latitude: 28.9°N) and the Xinglong (XL) station (40.2°N, 117.4°E, Magnetic Latitude: 30.5°N) in central China during the St. Patrick’s Day storm (from Mar. 17 to Mar. 19) of 2015 to analyze thermospheric wind disturbances and compare observations with the Horizontal Wind Model 2007 (HWM07). The results reveal that the wind measurements at KL show very similar trends to those at XL. Large enhancements are seen in both the westward and equatorward winds after the severe geomagnetic storm occurred. The westward wind speed increased to a peak value of 75?m/s and the equatorward wind enhanced to a peak value of over 100?m/s. There also exist obvious poleward disturbances in the meridional winds during Mar. 17 to Mar. 19. According to the comparison with HWM07, there exist evident wind speed and temporal differences between FPI-winds and the model outputs in this severe geomagnetic storm. The discrepancies between the observations and HWM07 imply that the empirical model should be used carefully in wind disturbance forecast during large geomagnetic storms and more investigations between measurements and numerical models are necessary in future studies.     

微振动对干涉仪运动机构均匀性的影响分析

外界振动对双角镜摆臂式傅里叶变换干涉仪（下简称干涉仪）运动机构速度均匀性的影响,可以通过干涉仪光程差速度稳定度来定量分析。文章针对空间光谱探测过程中,在轨微振动影响下的干涉仪运动机构可靠性问题,提出了一种更全面的光程差速度均匀性分析方法。该方法将外界激励引起的干涉仪结构响应作为一项影响因素纳入到稳定性的分析中,从而能够更真实地反映干涉仪在轨工作的可靠性,更准确地判断干涉仪能够承受的微振动临界。文章论述的方法为外界激励扰动下机构运动可靠性的判断以及机构控制优化的研究提供了一种思路。     

空心角隅棱镜在激光干涉测角中的应用

阐述了激光小角度测量装置中使用的实心角隅棱镜由于制造和安装误差对测量结果所造成的影响,同时提出利用空心角隅棱镜可以解决问题的理论依据,通过应用实验效果对理论给予验证.     

Modeling and Simulation of Pipeline Security Monitoring System Based on Line-Structure Sagnac Interferometer with 3×3Coupler

The third damage action,human disruption behavior,is one of the major threats to pipeline operation.It is necessary to monitor and locate the perturbation behavior that may threat pipeline safety in real-time.Therefore,a new pipeline security monitoring system is designed by using line-structure Sagnac optic fiber interferemeter with the characteristic of 3×3coupler that can modulate the phase of optic signal,with no need for phase modulation and demodulation.The optic structure of the new system is simplified,the signal processing accuracy is improved,and the polarization effect is reduced.The working principle of the monitoring in ideal condition is described,the phase demodulation is analyzed and the location of the possible damage action point is formulated.By using simulink,the optic signal propagation and interference is simulated and interference signals in different frequencies are obtained.The results validate the feasibility of the monitoring system and indicate that the low frequency signal less than 1kHz resulting from the human damage action can be detected.The disturbance set at 10 km can be located by calculating the demodulation signal accurately over a long monitoring distance.     

星间相位干涉仪测角系统设计及精度分析

针对微小卫星编队飞行、星间组网等多星协同任务中的相对测角问题,提出了一种高精度的星间无线电测角系统。该系统的优势是在伪码测距系统的基础上增加两条相同的接收通道,对载波相位值采用相位干涉法得到高精度的星间相对角度值,可以在不增加额外软硬件开销的情况下完成实时性较好的高精度星间相对状态自主测量。从该系统的设计出发,对相位干涉仪测角系统进行了详细的精度分析,推导了链路中各个噪声源的传递函数和理论噪声水平,并搭建实物平台对角度测量精度的理论值和实测值进行比较。结果表明系统对本振相位噪声有抑制作用,热噪声是角度测量的最大噪声源,系统实际测角精度在强信号下可达1.4×10^-3度。     

冷原子干涉型重力仪的发展现状与趋势

地球重力场反映了地球物质分布及其随时间和空间的变化.高精度重力加速度测量可以广泛应用于地球物理、资源勘探、地震研究、重力勘察和惯性导航等领域.冷原子重力仪是近二十年来快速发展起来的一种新型量子传感器,它利用激光冷却、原子干涉等技术实现高精度、高灵敏度的重力加速度测量.本文介绍了冷原子重力仪的发展历史、现状及趋势,详细论述了冷原子重力仪的原理、分类、装置及步骤等,并重点分析了小型化冷原子重力仪的关键技术.     

激光干涉仪远程触发功能及其在工作台运动性能评估中的应用

本文介绍了激光干涉仪远程触发端口的应用方法。根据测试要求，将实际触发信号经过分频，以满足激光干涉仪所能接受的频率；同时设计了移位叠加的方法完成全行程的小间隔的自动测量，为工作台运动评估和控制性能的改善提供了依据。     

用于铷原子磁光阱的超高真空系统设计

上抛式冷原子干涉重力仪,以Rb原子作为操控介质,使其在二维磁光阱中被冷却,在三维磁光阱中装载并在干涉区内实现探测。根据重力仪对真空系统的特殊要求,对真空系统的结构和参数进行设计,完成真空泵、真空腔室结构及光学玻片等关键部件的选型及设计,设计出结构紧凑实用的超高真空系统。在后期磁光阱的装配中,提出了相应的关键工艺技术,实现了超高真空系统的组装搭建。通过差分管的设计,二维磁光阱的真空度控制在10-6Pa,三维磁光阱的极限真空度达到10-8Pa。     

编队飞行卫星在间断式导航、天基干涉仪和分工式工作星的可行性构想

对将编队飞行卫星应用于用户间断性三维无源自主定位导航 ,用干涉仪对敌方目标被动定位和卫星分工式工作的可行性进行初步分析对比研究 ,除指出这些构想的队形要求和优点外 ,同时也给出其缺点和存在的困难