ls

实现时分秒的计数和校正实现时分秒的计数和校正(Realized and correction of minutes and seconds count)

请点击1.m运行文件（运行环境为matlab2008a） 注：不可直接运行1.fig 需使用1.m文件 附：输入各设备及物流量子窗口参数信息说明：请依次输入该零件所需的设备号，两个y设备号之间填入这两个设备间的物流量，例如一个零件需要的设备一次为3，5，7，其中3和5的物流量为10，5和7的物流量为20，则应按如下的格式输入3，10，5，20，7。只需输入数字即可，无需输入标点符号。且零件的排序为最下面的一行为零件1，向上依次递加。">

基于simulink的节气门控制算法设计 文档资料的 实际simulink 文件(Simulink based throttle control algorithm design the actual Simulink file of document data)

二维经验模态分解，采用形态学求极值点，径向基神经网络拟合，速度较快。(Two-dimensional empirical mode decomposition, the use of morphology for extreme points, Radial Basis Function Neural Network Fitting, faster.)

运筹学模型的MATLAB实现，附有程序源码(MATLAB realization of operations research model, with program source code)

自适应线性增强程序，Matlab代码，LMS算法(Application Program to Test Adaptive Line Enhancer )

This script illustrates the fading in gmsk under nakagami distribution.A reference paper is also included.

用四元数法的捷联惯性导航姿态解算程序。可以快速准确得到数据。(With the quaternion method Inertial attitude solver. You can get fast and accurate data.)

Print file from matlab to pdf or eps

fs = 8000 t = (0:1/fs:1). x1 = cos(2*pi*t*300) x2 = cos(2*pi*t*400) ha = phased.ULA( NumElements ,10, ElementSpacing ,1) ha.Element.FrequencyRange = [100e6 300e6] fc = 150e6 x = collectPlaneWave(ha,[x1 x2],[10 20 45 60] ,fc) rng default noise = 0.1/sqrt(2)*(randn(size(x))+1i*randn(size(x))) hdoa = phased.ESPRITEstimator( SensorArray ,ha,... OperatingFrequency ,fc) doas = step(hdoa,x+noise) az = broadside2az(sort(doas),[20 60])