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example4_5
分析双极性不归零码的功率谱特性请输入随机序列的长度N= (ubplot(312)
plot(f,lpf)
title( 低通滤波器 )
axis([-fs/2 fs/2-0.2 1.2])
subplot(313)
plot(f,abs(yr_lpf)/N)
title( 经低通滤波后的频谱 )
xlabel( f /Hz ) )
- 2010-05-25 20:56:23下载
- 积分:1
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mimo
mimo信道建模,仿真结果,信道建模介绍详细说明(mimo channel modeling, simulation results, detailed description of the channel model introduced)
- 2010-05-17 18:10:25下载
- 积分:1
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fre
关于详细介绍瞬时频率计算相关理论的文章,文章中已附有MATLAB程序(Detailed calculation of the instantaneous frequency of articles related to theory, the article with a MATLAB program has been)
- 2011-12-18 09:10:48下载
- 积分:1
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DISSERTATION
matlab code for A Novel Approach to Design and Implement
Dierential Time Lapse Video in Real Time
Application
- 2012-01-26 14:15:18下载
- 积分:1
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Henon
用来画荷农吸引子
离散系统的相轨迹图
二维系统(Farmers used to draw charge attractor the phase trajectories of discrete two-dimensional systems)
- 2010-11-10 10:51:30下载
- 积分:1
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line_inter_2d
Matlab的M文件编写的数控插补2D直线算法仿真。具体参数可使用:X-500,Y-600,Fc-600,Fs-0,Fa-0,at--200.仿真的本意是为了验证DSP上同类插补算法的正确性(Matlab M-file to prepare the CNC interpolation algorithm for 2D simulation of a straight line. Specific parameters can be used: X-500, Y-600, Fc-600, Fs-0, Fa-0, at- 200. The simulation is intended to verify the DSP on the correctness of the same interpolation algorithm)
- 2009-05-24 19:06:32下载
- 积分:1
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Dade_Toonify
matlab files to perform toonification on images using bilateral filtering
- 2013-10-23 21:01:34下载
- 积分:1
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math_exp
内容包括:插值与拟合实验,代数方程组的解法,微分方程实验,优化问题实验,综合实验(Include: interpolation and fitting the experimental, the solution of algebraic equations, differential equations experiment, optimization experiments, comprehensive experimental)
- 2010-11-05 15:59:22下载
- 积分:1
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blind4qamvs
这是一个恒模算法和变长恒模算法收敛性比较的程序.(This is a constant modulus algorithm and variable-length constant modulus algorithm to compare the convergence process.)
- 2009-07-09 23:45:59下载
- 积分:1
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Missile-Attitude-control
1、利用simulink中sfunction方法建立航天器姿态动力学模型和运动学模型;
2、利用linmod对非线性模型线性化;
3、姿态模型线性化后,利用极点配置(pole)方法求取控制参数;
4、将控制参数带入非线性模型仿真控制效果。(One using simulink sfunction method to establish the dynamic model and kinematic model of the spacecraft attitude
2, the use of linmod linearization of the nonlinear model
Attitude model linearization, the use of pole configuration (pole) is used to obtain the control parameters
4, the control parameters into the nonlinear model simulation control effect.)
- 2012-04-11 08:51:59下载
- 积分:1