锥面共形阵列极化-DOA估计的降维MUSIC算法

针对传统MUSIC(multiple signal classification)算法在锥面共形阵列极化-DOA(direction of arrival)参数联合估计过程中计算复杂度较高的问题,利用单极化阵元构造极化敏感锥面共形阵列,并建立阵列接收信号模型.通过构造同极化接收子阵,将导向矢量中空域信息和极化域信息去"耦合",在考虑阵元遮挡效应的条件下,结合秩损原理实现了基于降维MUSIC算法的极化-DOA多参数估计,减小了极化-DOA参数估计的计算量.通过计算机仿真证明了方法的有效性.     

Ultra-low latency and omit-iteration CORDIC algorithm

The pipeline structure Coordinate Rotation Digital Computer (CORDIC) algorithm improves its precision by increasing the stages of iterations, which leads to a large delay, excessive consumption of hardware and limits its applications.The omit-iteration CORDIC algorithm is proposed to solve this problem by using the methods of binary to bipolar recoding, folding angle domain, merging iteration and optimizing the lookup table. Simulation results show that this method needs only two clock cycles to get the output and also makes improvement on the hardware consumption and its precision, especially having privilege to the application on high speed and real-time occasions compared with other realization of the CORDIC algorithm.     

基于FPGA的瞬态响应测试仪的设计与实现

为提高瞬态响应测试仪的测量精度和响应速度,提出了一种基于现场可编程门阵列(FPGA)实现的设计方法.系统设计采用Xilinx公司生产的Xilinx Spartan 3E XC3S500E PQ208 FPGA作为控制核心,实现了对瞬态响应的峰值时间、超调量及调节时间的精确测量,并且能较准确地绘制二阶系统的瞬态响应曲线.系统显示模块采用VGA显示,既节约了IO口资源,又可以更加逼真地显示相应曲线.系统可通过模拟开关实现单脉冲信号的输出,并扩展了语音提示功能,使用更方便.实际测试表明,系统具有运行稳定、参数测量精度高、抗干扰强及响应速度快的优点.     

基于加权平滑l_0范数的单快拍波达方向估计

针对现有基于压缩感知的DOA估计算法估计精度不高的问题,提出一种基于加权平滑l0范数的单快拍DOA估计算法。所提算法采用一种新的加权方式,在构造一个恰当的平滑连续函数后,根据接收数据的初始解确定一个合适的递减的{σ}序列[σ_1,σ_2,?,σ_J],并对每一个σ值,用最速下降法来求解l0范数的逼近函数H_σ(S)的最小值;然后将该σ值作为下一次迭代的初始值,并在每次迭代开始时更新权值,通过多次的迭代获得逼近函数的最小解,即逼近的最小l0范数。通过仿真实验表明所提算法可对DOA进行有效估计,且容易实现、精度较高,与未加权的改进平滑l_0范数DOA估计方法相比具有更好的估计性能。     

共形阵列MUSIC算法分辨力性能分析

针对共形阵列分辨力性能分析问题,本文首先对锥面、柱面、球面等3种常见共形阵列进行信号建模,并基于MUSIC算法实现共形阵列下极化-DOA参数的联合估计,然后通过MUSIC零谱的定义以及噪声子空间投影矩阵的期望,给出MUSIC期望谱的具体表现形式,在此基础上详细分析推导了MUSIC算法在共形阵列中的分辨力门限;最后通过计算机仿真研究共形阵列分辨力门限理论值与仿真值的关系,以及共形阵列与均匀圆阵在分辨力性能上的差异,仿真结果显示共形阵列的分辨力门限随着信噪比的增加逐步降低,验证了理论分析的正确性.     

联合DOA估计与主波束形成的干扰抑制方法

为克服测距仪(DME)发射的高强度脉冲信号干扰L频段数字航空通信系统1(L-DACS1)OFDM接收机的问题,提出联合DOA估计与主波束形成的干扰抑制方法.首先接收机通过波达方向矩阵算法估计接收信号来向;然后基于信号来向通过线性约束最小方差波束形成算法提取各个方向信号;随后通过频域功率与时域功率比较算法分辨各来向信号的类型;最后输出OFDM直射径信号.仿真结果表明:该方法可显著克服DME与OFDM散射径信号干扰,提高L-DACS1系统链路传输的可靠性.     

卫星太阳翼板面水平展开试验方法

为减少卫星姿态翻转,确保卫星光学载荷指向精度,提出卫星太阳翼板面水平展开试验方法.采用多自由度配重悬挂法抵消太阳翼水平展开试验过程中的重力,开展运动学及动力学分析、试验误差分析,完成卫星太阳翼板面水平展开试验验证.试验结果表明:相比传统展开试验方法,能够更真实的模拟太阳翼在轨展开运动;对太阳翼配重质量偏差、太阳翼吊挂质心偏差及系统摩擦力控制要求高.验证模型和试验方法的正确性,满足卫星太阳翼展开试验要求.     

New LED light source system with uniform illumination for line-scan CCD imaging systems

A system with uniform light reflection in the inner surface within a horizontal 2/3 cylindrical structure for line-scan CCD of the print testing was designed. The design was based on diffuse reflection uniformity of the integrating sphere and requirement of the strip uniform illumination region. This system was called dome light. White light LED array light sources were used for uniform illumination. The LEDs were filtrated to composite array light source based on coefficient of variation of a single LED. The standard white board and SG color checkers were used in the line-scan CCD imaging experiments under the dome light and ordinary illumination light source. The average color difference (ΔE) of SG color checkers in CIELAB space was 2.091 under the dome light and 2.286 under ordinary illumination light source respectively. Experimental results indicate that the dome light can satisfy illumination uniformity and color rendering consistency for line-scan CCD and provide a standard light source for uniform calibration of different cameras.     

Low complexity SEU mitigation technique for SRAM-based FPGAs

An internal single event upset (SEU) mitigation technique is proposed, which reads back the configuration frames from the static random access memory (SRAM)-based field programmable gate array (FPGA) through an internal port and compares them with those stored in the radiation-hardened memory to detect and correct SEUs. Triple modular redundancy (TMR), which triplicates the circuit of the technique and uses majority voters to isolate any single upset within it, is used to enhance the reliability. Performance analysis shows that the proposed technique can satisfy the requirement of ordinary aerospace missions with less power dissipation, size and weight. The fault injection experiment validates that the proposed technique is capable of correcting most errors to protect space-borne facilities from SEUs.     

完备局部凸凹计数模式及其旋转不变纹理分类

局部凸凹模式是新近提出的一种有效纹理描述子,但对旋转纹理图像描述不足。针对局部凸凹模式算法的此缺陷,提出了局部凸凹计数模式进行旋转不变纹理描述。局部凸凹计数模式统计纹理的局部凸或凹模式数目,而抛弃了局部凸凹模式的结构信息。在纹理图像发生平面内旋转情况下,局部凸凹计数模式所提取的纹理特征具有不变性。另外,为了增强局部凸凹计数模式的性能,提出了完备局部凸凹计数模式算法。完备局部凸凹计数模式不仅统计了局部凸或凹模式数目,还对局部纹理的凸或凹强度进行了描述,中心像素所包含的鉴别信息也统计在完备局部凸凹模式算法中。二个纹理数据库和一个掌纹数据库上的试验充分表明完备局部凸凹计数模式是一种有效的旋转不变纹理特征提取算法。