登录
首页 » matlab » 105230333MODULATION

105230333MODULATION

于 2009-05-20 发布 文件大小:34KB
0 233
下载积分: 1 下载次数: 6

代码说明:

  matlab GMSK modulation

下载说明:请别用迅雷下载,失败请重下,重下不扣分!

发表评论

0 个回复

  • Chapter44
    MATLAB 小波分析高级技术——书中的一些应用程序(MATLAB senior technical wavelet analysis-- Some of the applications)
    2006-07-05 21:26:41下载
    积分:1
  • OR
    说明:  OR规则下载,可以根据自己的想法添加元素(OR download the rules, you can add elements according to their own ideas)
    2011-06-22 12:38:44下载
    积分:1
  • MATLAB
    matalb图像处理基础源代码,整理版,可以实图像变换的一些基本功能(matalb based image processing source code, finishing version, you can actually change some of the basic functions of image)
    2011-10-07 00:21:20下载
    积分:1
  • shuzixinhaochulishiyancxu
    数字信号处理实验程序部分,配对我发布的数字信号处理实验讲义,基于Matlab的FFT变换,IIR数字滤波器设计,FIR数字滤波器设计(Digital signal processing part of experimental procedure, matching my release digital signal processing experiment notes, based on Matlab' s FFT transform, IIR digital filter design, FIR digital filter design)
    2010-06-18 18:18:26下载
    积分:1
  • 36331-b40
    3GPP组织给出的LTE系统高层无线资源控制RRC层规范,希望帮到LTERRC层爱好者。(3GPP LTE system tissue senior radio resource control (RRC) layer specification given, I hope to help LTERRC layer enthusiasts.)
    2014-01-08 16:29:30下载
    积分:1
  • exa060302
    利用单带滤波器来设计一个半带滤波器,并显示半带滤波器H0,H1,及 H0+H1的幅频响应 单带滤波器的归一化截止频率为0.84,长度=16,半带滤波器的长度=31。(to explain how to design a biorthogonal FB by Lattice structure)
    2009-11-05 10:44:50下载
    积分:1
  • MATLAB_PDE
    偏微分方程的MATLAB解法,包括偏微分方程工具箱,图形用户界面,典型方程及实用例子,工具箱命令,有限元和有限差分法常微分方程解法(matlab solutions for partial differential equation )
    2013-02-03 16:48:06下载
    积分:1
  • svr-m
    舵机 伺服马达的连线介绍,控制信号,工作电压 图解(Steering servo motor connected introduction, the control signal, operating voltage diagram)
    2011-12-22 12:53:59下载
    积分:1
  • orbit
    编程仿真连续小推力实现GTO到GEO的三阶段转移过程,其中推力器的推力大小为0.8N,轨道机动的起始点为GTO的远地点。GTO轨道的升交点赤经为0度,近地点角距为90度。 GTO轨道: ph:185km,ah:35786km,i:28.5°,GEO轨道:h:35786km,i:0°。 卫星质量为6600kg,从GTO到GEO,采用5000s的推力器。取地球半径为6378km,g取值为9.8m/s^2(The three stage transfer process from GTO to GEO is realized by simulation and continuous small thrust. The thrust of the thruster is 0.8N, and the starting point of orbital maneuver is the apogee of GTO. GTO orbit RAAN is 0 degrees, 90 degrees for the argument of perigee. GTO orbit: ph:185km, ah:35786km, i:28.5, GEO orbit: h:35786km, i:0. The mass of the satellite is 6600kg, from GTO to GEO, using the 5000S thruster. The radius of the earth is 6378km, and the value of G is 9.8m/s^2)
    2021-01-28 10:38:35下载
    积分:1
  • Radar.Systems.Analysis.Using.MATLAB
    用matlab实现雷达系统仿真 pdf电子书 英文版 原理讲解和代码(Radar systems analysis and design using matlab, pdf e-book in English to explain the principles and code)
    2011-11-10 15:23:24下载
    积分:1
  • 696518资源总数
  • 106148会员总数
  • 10今日下载