登录
首页 » Visual C++ » fir_lp

fir_lp

于 2012-11-21 发布 文件大小:1KB
0 258
下载积分: 1 下载次数: 6

代码说明:

  1. To design FIR filters in MATLAB to achieve various types of frequency selectivity, e.g., lowpass, highpass,bandpass, etc 2. To verify the frequency response of the designed filters in MATLAB 3. To implement the designed FIR filters using C6713 DSK and 4. To perform real-time testing of the performance of the designed FIR filters.

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

  • Matlab-and-cPP-programming
    精通Matlab与C/C++ 混合程序设计(第2版)(Proficient in Matlab and C/C++ mixed program design (2nd edition))
    2012-06-25 16:08:21下载
    积分:1
  • TestLocalHeap
    Windows Local heap class
    2014-11-30 22:26:27下载
    积分:1
  • qstoolbox
    该代码为排队论工具.用于MM1,MG1等模型. (code for the queuing theory tools. For MM1, genotoxicity and other models.)
    2007-01-16 19:53:20下载
    积分:1
  • up
    说明:  简单例子A simple exampleA simple example(A simple example)
    2014-10-22 13:13:14下载
    积分:1
  • FFTchangefilter
    DFT数字信号采集滤波器实例演示程序,很实用的一个小程序。(DFT filter digital signal acquisition example demo program, it is a small utility program.)
    2007-10-22 23:13:53下载
    积分:1
  • inption1
    matlab和VC混合编程的数据n倍内插处理系统,混编使用matcom代码转换方式实现(matlab and programming VC mixed data n times the interpolation processing system, mixed use Matcom realize the code conversion mode)
    2008-07-02 20:09:40下载
    积分:1
  • VideoGameTheory
    Video Game Theory to develop game
    2014-01-22 09:37:53下载
    积分:1
  • Idegnwenxians
    等温线,matlab等温线经典程序,内置数据-IIsotherms , (The isotherm, matlab isotherm classic program, built-in data-IIsotherms,)
    2012-08-22 14:41:32下载
    积分:1
  • han1
    这里我们针对三级固体火箭进行研究,主要考虑每一级发动机工作时推力 和比冲 与发动机试车存在摄动偏差(相差 )时所产生火箭关机点时刻的状态偏差。火箭的飞行的动力学方程可建立在地面发射坐标系中,火箭的第一级、第二级和第三级按照固定的俯仰角程序飞行,第二、三级飞行时已在大气层外,此时可忽略气动力的影响。(Here we study for three solid rocket, the main consideration at every level when the engine thrust and state arising the moment the rocket off point perturbation deviation (difference) in the presence of specific impulse and engine test bias. Outside of the rocket flight dynamics equations can be established on the ground coordinate system launch, the rocket s first stage, the second and third stages according to a fixed elevation angle of flight procedures, and the second, when the third flight already in the atmosphere, this when can ignore the effects of gas dynamics.)
    2020-11-03 20:39:53下载
    积分:1
  • NLSEmagic
    用c语言和matlab联合编程求解非线性薛定谔程序,应用CUDA并行技术(nonlinear schrodinger equation solver)
    2016-07-06 17:01:38下载
    积分:1
  • 696516资源总数
  • 106914会员总数
  • 0今日下载