登录
首页 » matlab » sequence-of-DTFT-analysis

sequence-of-DTFT-analysis

于 2011-05-30 发布 文件大小:457KB
0 191
下载积分: 1 下载次数: 13

代码说明:

  matlab的有限长序列的DTFT分析 matlab的有限长序列的DTFT分析(Matlab limited long sequence of DTFT analysis)

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

  • local_histeq
    local histogram maching
    2010-12-16 23:55:18下载
    积分:1
  • 294976fcm
    this is also fuzzy c means clustering for segmentation
    2013-09-19 17:48:38下载
    积分:1
  • fft
    here a file to computee fourier tranform of an image
    2014-12-18 15:12:19下载
    积分:1
  • IEEE80211b_PHY_DBPSK
    ieee802.11b m-file for simulation this link. this file includes the manner for using barker codes in wireless communication
    2012-02-08 14:38:17下载
    积分:1
  • kfvsskf
    该Matlab程序给出了Schmidt-Kalman filter和标准Kalman filter之间的性能对比,不是函数的形式,是直接的可执行程序,如有需要,直接更改文件中的参数就可以了(The Matlab program gives the Schmidt-Kalman filter and standards of performance comparison between the Kalman filter is not a function of the form is directly executable program, if necessary, change the file directly to the parameters can be a)
    2009-12-19 13:26:55下载
    积分:1
  • t2controlchart
    利用matlab計算t2管制圖phase1的管制上限及管制下限(Calculated using matlab control t2 control chart phase1 upper and lower control)
    2011-06-17 13:53:58下载
    积分:1
  • MIMO_ALLOCTION
    该文档描述了MIMO-OFDM系统中关于资源分配算法的具体仿真方法,对于初学者有很大作用。(This document describes the specific MIMO-OFDM system simulation method for resource allocation algorithm plays a significant role for beginners .)
    2014-02-22 20:16:59下载
    积分:1
  • marcv
    说明:  利用ode45求解微分方程组。利用马尔可夫状态转移,求解系统部件随时间的可靠性函数。(Use matlab to solve system of differential equations.)
    2021-04-15 20:58:54下载
    积分:1
  • fuzzy_manupulator
    a matlab model of a fuzzy controlled 2-link manipulator
    2009-11-25 02:04:27下载
    积分:1
  • Satellite_orbit_design
    现需要在高度为600~700KM范围内,回归周期为30天的太阳同步轨道上布置一颗L波段的合成孔径雷达卫星。 1. 请设计合适的轨道参数,并仿真对应轨道下一个运行周期内星下点轨迹图(纬度和经度两个图); 2. 计算多普勒中心频率,多普勒调频率与纬度的关系图(设姿态角为0°,天线视角20°~60°,推荐35°); 3. 按高斯投影方式,将星下点轨迹图投影到地图坐标上。(Now requires a height of 600 ~ 700KM range, return period of 30 days are arranged on a sun-synchronous orbit L-band Synthetic Aperture Radar satellites. 1 Please design the appropriate orbital parameters and simulate the corresponding orbit within the next operating cycle nadir trajectories (latitude and longitude two graphs) 2. Calculate the Doppler center frequency, Doppler frequency and the relationship between latitude Figure (set attitude angle is 0, the antenna angle of 20 to 60, recommended 35) 3 Press Gauss projection, the nadir trajectories projected onto the map coordinates.)
    2013-07-19 14:56:28下载
    积分:1
  • 696516资源总数
  • 106562会员总数
  • 4今日下载