稳态等离子体推力器羽流仿真及其对微波的衰减和相移作用

为了评估稳态等离子体推力器（SPT）羽流对微波造成的衰减和相位变化,使用二维轴对称的PIC-DSMC方法,在空间及室压6mPa的真空舱两种环境下,计算了SPT-100羽流场中的电子分布。在此基础上,通过分析特征频率和计算衰减因子、相位常数,估算了2,4,8,12.5GHz共4个频率微波穿过羽流场时的衰减量和相移。8GHz和12.5GHz微波未发现明显的衰减,相移为10°～120°。2GHz和4GHz微波在喷口附近衰减量范围为10～50dB。仿真结果表明,C波段和S波段在SPT羽流中容易发生衰减,而X波段以上的高频微波衰减量很小,同时这几个波段微波均发生较大相移。真空舱内6mPa背压下对衰减量的预测仅略高于实际飞行情况,但微波相移会有较大误差。     

地面模拟微重力条件下Cu-Pb合金的制备及微观结构与摩擦性能研究

利用地面上建立的微重力电磁模拟设备成功制备出了Cu-Pb二元难混合金,并对其微观组织结构与摩擦性能进行了分析与测试。样品SEM分析结果表明,模拟微重力状态下制备的合金样品较好地克服了地面上因重力影响而产生的严重成分偏析,少数弥散相较均匀地分布于基体中,少数相含量越低,弥散体尺寸越小,分布越均匀;摩擦性能测试结果显示合金模拟样品的摩擦性能明显好于基体金属,且摩擦系数随少数相Pb的含量的增大而减小,体积磨损率随少数相含量的增大先快速减小而后又缓慢增大。同时对实验结果进行了简单的分析与讨论。      

池沸腾现象中热毛细对流的成因

针对微重力条件下单组份液体池沸腾现象,探讨了有关热毛细效应作用及其成因的不同观点,指出正确描述气液相变界面两侧的温度关系是解决争议的关键.详细评述了现有的气液相变界面温度模型,发现气液相变的非平衡特征会导致气液界面上产生温度梯度,引起表面张力的显著差异,从而驱动热毛细对流的形成.但现有气液相变界面温度模型机理差异迥然,预测结果也差别很大,因此,需要更深入研究.      

基于ADF4153的频率合成器设计

设计实现一种基于ADF4153的频率合成器,介绍该频率合成器的构成原理。结合测试结果对本频率合成器进行相位噪声性能分析和杂散分析,并提出相应的改善措施。利用软件仿真对环路的稳定性进行分析。测试及分析结果表明,本频率合成器相位噪声水平可达-96.59dBc@10kHz,杂散抑制大于45dBc,频率合成器环路工作稳定。     

谐振式加速度计自激振荡电路性能评价方法的研究

针对谐振式加速度计成品率不高、精度低等问题,以石英振梁加速度计为例,采用引进标准信号,将谐振电路作为"黑盒子",对其开展独立的评价.通过评价电路的驱动电压幅值稳定性、移相稳定性、全温幅值/相位对称性等指标,与加速度计实际指标建立了一一对应的关系,为加速度计研制与性能提升提供了有效依据.实际运用表明,电路噪声性能、温度性...     

Imaging of target with complicated motion using ISAR system based on IPHAF-TVA

The technique of imaging a target with a complicated motion using an Inverse Synthetic Aperture Radar (ISAR) system is an effective tool in the field of radar signal processing. After the translational compensation, the received signal reflected from the target can take the form of a multi-component Polynomial Phase Signal (m-PPS), and the high quality ISAR image can be provided via the combination between the estimated parameters of the m-PPS and the Range Instantaneous-Doppler technique (RID). For a target with a high maneuvrability, the occurrence of scatterers Migration Through Resolution Cell (MTRC), caused by the rotational movement could be appearing. That is why the variation in the amplitude of the echo during the time of observation cannot be neglected. The purpose of this study is the parameters estimation of the m-PPS signal with order three in the case of the Time Varying Amplitude (TVA). The Improved-version of the Product High-order Ambiguity Function (IPHAF) with TVA is proposed to improve the quality of the ISAR image compared with traditional techniques based on a constant amplitude; the experimental outcomes confirm that the new IPHAF-TVA method presented in this study is an effective technique to make the ISAR image very clear.     

中继卫星系统仿真软件设计与应用*

设计开发中继卫星系统仿真软件,并针对理想信道条件、I/Q幅相不平衡、幅频特性、群时延、相位噪声、功放饱和条件、非线性信道条件这七种信道,仿真16QAM和16APSK的误码率性能,并对仿真结果进行分析。利用仿真平台得出的非线性信道条件下误码率需求与所需信噪比之间的关系,可以作为完善系统技术指标的重要依据,为中继卫星系统后续建设和应用提供重要参考。     

Spaceborne GPS receiver antenna phase center offset and variation estimation for the Shiyan 3 satellite

In determining the orbits of low Earth orbit (LEO) satellites using spaceborne GPS, the errors caused by receiver antenna phase center offset (PCO) and phase center variations (PCVs) are gradually becoming a major limiting factor for continued improvements to accuracy. Shiyan 3, a small satellite mission for space technology experimentation and climate exploration, was developed by China and launched on November 5, 2008. The dual-frequency GPS receiver payload delivers 1 Hz data and provides the basis for precise orbit determination within the range of a few centime-ters. The antenna PCO and PCV error characteristics and the principles influencing orbit determi-nation are analyzed. The feasibility of PCO and PCV estimation and compensation in different directions is demonstrated through simulation and in-flight tests. The values of receiver antenna PCO and PCVs for Gravity Recovery and Climate Experiment (GRACE) and Shiyan 3 satellites are estimated from one month of data. A large and stable antenna PCO error, reaching up to 10.34 cm in the z-direction, is found with the Shiyan 3 satellite. The PCVs on the Shiyan 3 satellite are estimated and reach up to 3.0 cm, which is slightly larger than that of GRACE satellites. Orbit validation clearly improved with independent k-band ranging (KBR) and satellite laser ranging (SLR) measurements. For GRACE satellites, the average root mean square (RMS) of KBR resid-uals improved from 1.01 cm to 0.88 cm. For the Shiyan 3 satellite, the average RMS of SLR resid-uals improved from 4.95 cm to 4.06 cm.     

基于软件锁相环的电机速度控制系统

随着电力电子、微电子技术和控制技术的发展，一些场合对电机调速系统性能的要求越来越高，而锁相调速控制在稳速精度方面有其独特的优势。文章在改进的数字锁相环基础上，提出了软件锁相环电机速度控制系统，利用高性能微处理器实现了软件锁相环。     

具有星间链路的星座相位设计

通过分析星座空间构形的变化规律，综合考虑星座空间构形对地面覆盖特性、星间链路、空间测量精度以及工作性能的影响，利用改进的层次分析法对星座相位进行优化设计。通过对全球覆盖星座进行仿真，验证了方法的可行性。