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CODE-FIX
ARRUAM CODIGO NO VISUAL BASIC
- 2014-08-20 00:54:03下载
- 积分:1
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201203003_3_Assignment
This describes two ways of rotating an image
1. With black dots in between
2. Clear image received after enlarging then rotating then reducing size again
- 2013-02-09 02:50:52下载
- 积分:1
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lmsalgorithm
信道估计中的LMS算法matlab程序,希望对大家有所帮助(LMS channel estimation algorithm matlab program, we want to help)
- 2010-07-09 17:30:59下载
- 积分:1
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rddata
Matlab function to read ECG signals.
- 2011-01-17 22:16:53下载
- 积分:1
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WSCC_9_bus_system
模拟WSCC 9公交系统。我已经做了这个系统与标准数据。如何在Matlab环境下对模拟输电线路的参数(电阻、电抗和电纳)是由分布参数与平衡负载流。千瓦&千乏的发电机的参数转换成KVA和Matlab仿真千伏。(This simulation is of WSCC 9 Bus System. I have made this system with standard datas. How ever for simulating in Matlab environment the parameters of transmission lines ( Resistance , Reactance and Susceptance ) are taken by distributed parameters with balance load flow. The Parameters of generators in KW & KVAR are converted into KVA and KV for Matlab simulation. )
- 2014-11-19 23:35:42下载
- 积分:1
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Lifting9-7
沙威的97小波变换程序,具体97小波的资料,大家可以下载相关论文。(shawei s 97 lifting wavelet transforming program code)
- 2010-08-22 16:52:47下载
- 积分:1
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tuxiangfenge
说明: 利用类间方差阈值算法实现图像的分割处理;利用形态学处理进行处理结果修正。
(Threshold using Otsu algorithm image segmentation use of morphological processing for processing the results of correction.)
- 2011-04-11 16:48:03下载
- 积分:1
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lowpass
实现低通滤波器,可以与PRony分析搭配使用,滤除信号中的高频分量。(Low-pass filter used in conjunction with the PRony analysis to filter out high frequency components in the signal.)
- 2012-05-23 19:34:01下载
- 积分:1
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Encryption
Matlab image encryption
- 2015-02-20 13:12:31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