SRAM型FPGA的抗SEU方法研究

通过分析静态随机访问存储器(Static Random Access Memorg,SRAM)型现场可编程门阵列(Field Programable Gate Array,FPGA)遭受空间单粒子翻转(SEU)效应的影响,并比较几种常见的抗SEU技术:三模冗余(Triple Module Redwcdancy,TMR)、纠错码(Error Correction Code,ECC)和擦洗(Scrubbing),提出了一种硬件、时间冗余相结合的基于双模块冗余比较的抗SEU设计方法。在FPGA平台上对线性反馈移位寄存器(Linear Feedback Shift Register,LFSR)逻辑进行软件仿真的抗SEU验证实现,将各种容错设计方法实现后获得的实验数据进行分析比较。结果表明,64阶LFSR的抗SEU容错开销与基于硬件的TMR方法相比,可以节省92%的冗余逻辑资源;与基于时间的TMR相比,附加时间延迟缩短26%。     

衰落信道中不同集分割的Turbo TCM方案的性能研究

比较了衰落信道下两种不同的集分割方式,UP（Ungerboeck分割）和BP（分组分割）对Turbo TCM性能的影响。研究了在两种不同映射以及不同帧长度下Turbo TCM的性能。并给出了在8PSK和8ASK两种调制方式下的仿真试验结果,通过比较得出了很有意义的结果。     

开源软件定制改造过程中的原型选择

在定制改造开发过程中选择合适的原型系统,可以达到提高定制改造过程效率、减少开发成本、缩短开发周期的目的.在定制改造过程的原型分析和评估中依托构造成本模型COCOMO(COstructive COst MOdel) II,提出一种新的软件成本评估方法,综合分析了影响定制改造过程的功能差异、性能、规模、稳定性等关键因素,量化了这些关键因素对定制改造过程中成本计算公式中的关键变量——等价代码——的影响.实际的项目显示,该方法对预期工作量的估计误差约为17%,远小于COCOMO II模型40%的可接受阈值.      

扩频数字接收机中的多相匹配滤波

文章提出一种改进形式的伪随机码匹配滤波器,这种改进形式将整数倍抽取、内插等重采样处理（重采样处理满足Nyquist采样定理）与伪随机码匹配滤波器相结合,用多相形式实现伪随机码的匹配运算。这种方法在改进原匹配滤波器并行处理结构的同时降低了对存储数据用的总的存储量要求和运算速率。     

基于FFT的伪码快速捕获算法研究

扩频通信系统对信号捕获性能的要求不断提高,文中研究一种基于FFT的伪码快速捕获算法。应用易于硬件实现的基2-FFT算法。为了得到2~N长序列。讨论补零、线性内插、邻近取值、sinc函数内插四种重采样方法,分析比较他们在捕获过程中时相关峰值计算结果的影响。其中sinc函数内插法可以得到最好的捕获效果。针对微弱和高比特率信号,详细介绍并分析一种多数据住相关值整合算法。仿真证明这种捕获算法可以提高微弱信号的检测性能。     

伪码-线性调频复合信号的参数估计

针对伪码随机二相编码-线性调频复合信号的参数估计问题,提出了基于解线调与相位差分的盲估计方法。首先对信号进行平方,消除相位调制,然后用解线调估计出调频斜率,用重构的线性调频信号消除复合信号中的线性调频成分,用平滑的功率谱估计出起始频率,最后采用改进的相位差分进行码元宽度的估计与伪码序列的恢复。仿真结果验证了方法的有效性。     

Unlicensed Spectrum Sharing Game Between LEO Satellites and Terrestrial Cognitive Radio Networks

By cognitive radio,the low Earth orbit(LEO) satellites may prefer to operate in the unlicensed spectrum which is open to all the users,and compete for the limited resources with terrestrial cognitive radio networks(CRNs).The competition can be regarded as a game and analyzed with game theory.This particular unlicensed spectrum sharing problem is modeled here,and the special properties of "spatially-distinguished-interference" and the short period of the interactions between satellites and terrestrial CRNs are explored.Then,the problem is formulated as a "partially-blind" finitely repeated prisoner’s dilemma by game theory.Finally,we begin with two promising spectrum sharing schemes,which can be used to enforce the frequency reuse among the remotely located terrestrial CRN players as well as to overcome the observation noise.By analysis and comparison,it is proposed that the novel refreshing-contrite-tit-for-tat(R-CTFT) is the optimal spectrum sharing scheme.Simulation results verify that it can be used to utilize the spectrum most efficiently.     

基于周期Wigner-Hough变换多相编码连续波雷达信号检测算法

为提高雷达侦察截获接收机对多相编码连续波弱信号截获能力,提出了一种基于周期Wigner-Hough变换（Periodic Wigner-Hough Transform,PWHT）的多相编码连续波信号检测算法。研究了线性调频连续波信号的PWHT及性质;分析了多相编码连续波信号时频主脊线的类似线性调频连续波特征;推导了高斯白噪声在PWHT域的统计分布特征,根据多相编码连续波信号与线性调频连续波的相似性,提出了基于PWHT的多相编码连续波信号检测算法,给出了实现流程,并计算出其检测性能和参数估计性能仿真的仿真结果。仿真结果表明：该算法较已有的其他多相编码信号检测算法有更好的弱信号检测能力,最小可检测信噪比至少可以降低3dB,并随着观测时间延长而进一步降低;其参数估计精度具有渐进最优的性质。     

基于原模图扩展的QC-LDPC构造方法

基于原模图构造的低密度奇偶校验码(LDPC)性能很大程度上取决于扩展算法。为此,提出了一种构造准循环低密度奇偶校验码(QC-LDPC)的新方法。所述算法经过两步扩展得到QC-LDPC:第一步是原模图去重边,在边置换条件的约束下,使扩展所得矩阵局部围长最大化;第二步进行准循环扩展,通过计算机搜索得到规定长度内的所有闭环路径,比较环长和近似环路外信息度得到置换矩阵的最优偏移量,目的是剔除连通性差的短环对码性能的负面影响。对于不存在重边的原模图,则直接进行准循环扩展。仿真结果表明,利用该方法构造的QC-LDPC在译码门限和误码平层两方面都具有优异的性能。     

Computations of unsteady transonic flow over airfoil at low Reynolds number

Transonic flow over a thin airfoil at low Reynolds number was studied numerically by directly solving two-dimensional full Navier-Stokes equations through 5th order weighted essentially non-oscillatory(WENO) scheme without using any turbulence model.A series of distinguished unsteady phenomena for a thin 2-D transonic airfoil flow were presented.Due to continuous adverse pressure gradient in the subsonic flow downstream of the sonic line, the unsteady separated boundary layer with main vortex and secondary vortex was developed at the rear of the airfoil.At the trailing edge,the vortex-shedding was characterized by periodical connection of the main vortex and secondary vortex on the other side of the airfoil.The unsteady separation and vortex-shedding occurred with the same period.On the airfoil surface,the average pulse pressure related to the unsteady supersonic region was obviously smaller than that related to the vortex-shedding at the trailing edge.With the attack angle increasing from 0° to 2°, the frequency of vortex-shedding decreases about 4.2%.At last, the turbulence intensity and many second-order statistics in the wake region were investigated.