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lab2
ec627 speech processing lab2 program
- 2009-10-25 02:10:27下载
- 积分:1
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MinimumCostFlow
说明: 最小费用最大流问题 MATLAB编程代码(Maximum flow problem minimum cost MATLAB programming code)
- 2009-08-13 18:20:01下载
- 积分:1
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model
用matlab判断验证产生的变量的各种分布情况(to estimate the ditribution)
- 2011-10-23 08:42:49下载
- 积分:1
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Application
信道编码技术在数字通信系统中的应用研究,主要针对卷积码进行了仿真。(Application of channel coding technology in digital communication systems, mainly for convolution codes simulated.)
- 2015-04-19 05:01:42下载
- 积分:1
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AP
AP算法源码代 运行可以画出图 AP算法源码代 运行可以画出图(AP algorithm source code to run on behalf of AP algorithm source code can be drawn diagram can be drawn map on behalf of running)
- 2013-08-15 14:56:28下载
- 积分:1
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MATLAB_shuzhifenxi
数值分析是一门比较实用的课程,在数学建模等方面应用广泛,这些代码里面几乎涵盖了全部的数值分析方法。(Numerical analysis is a more practical curriculum, widely used in mathematical modeling, etc., these codes which cover almost all of the numerical analysis method.)
- 2014-02-16 10:40:57下载
- 积分:1
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ROC
介绍了检验概率、虚警概率和信噪比之间的关系,并对其进行了仿真验证。(Inspection probability and false alarm probability are introduced and the relationship between the SNR, and the simulation verification.)
- 2016-03-11 14:33:01下载
- 积分:1
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RBFlw5
这是matlabdaima,用来计算RBF输出值很有效(This is matlabdaima, used to calculate the RBF output is valid)
- 2010-09-13 15:50:30下载
- 积分:1
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Wireless-Lab-2-----Plotting-Signal-Constellations
To plot a 16-QAM signal constellation with annotations that indicate the mapping integers to constellation points. The code uses the scatterplot function to create the plot and the text function in MATLAB to create the annotations. We follow the following steps for this.
- 2015-02-06 13:27:30下载
- 积分:1
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月球软着陆程序
说明: 月球软着陆仿真:在停泊轨道上,探测器在脉冲制动的作用下,经霍曼变轨,下降到距月面大约 15 公里的近月点,该近月点就是主制动段的初始制动点。主制动段以下是障碍检测与规避和最终着陆段。在主制动段,由于探测器的初始速度很大(1.692km/s),所以主制动段制导律设计的主要目的就是高效抵消此速度,将探测器导引到期望的末端状态(Lunar soft landing simulation: in the parking orbit, the probe under the action of pulse braking, through the hohmann change of orbit, to descend to about 15 kilometers from the surface of the moon, the near-moon point is the main braking section of the initial braking point. Following is the main braking section for obstacle detection and avoidance and the final landing section. In the main braking section, since the initial velocity of the detector is very large (1.692km/s), the main purpose of the guidance law design of the main braking section is to effectively offset this velocity and guide the detector to the desired terminal state)
- 2021-01-28 22:18:35下载
- 积分:1