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RPF
用MATLAC做的非线性时间序列预测和平滑,可以用来做非线性模型的预测和估计(MATLAC done using nonlinear time series prediction and smooth, non-linear model can be used to make the projections and estimates)
- 2007-12-06 21:35:21下载
- 积分:1
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EnergyDetection
Energey Detection ROC plot. Probablity of detection vs Probablity of false alarm.
- 2015-04-01 17:01:27下载
- 积分:1
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SR
说明: IBP matlab source code for super resolution application
- 2010-06-09 14:50:27下载
- 积分:1
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MATLAB7
MATLAB7.0课本所有程序清单,共37章,特别适合初学者,可以帮助节省大量时间,又能看到结果(MATLAB7.0 books list all the procedures, a total of 37 chapters, particularly suitable for beginners that can help save a lot of time, can see the result)
- 2008-08-06 17:17:37下载
- 积分:1
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Matlab_tutorial
说明: 详细说明matlab语言的语法结构,提供相应 信号处理的代码(Detailed description of matlab language grammar structure, and provide the appropriate signal processing code)
- 2008-08-30 14:51:47下载
- 积分:1
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matpower5.0b1
最新matpower 5.01工具箱,可以进行潮流、最优潮流、时域仿真等一系列计算。功能十分强大,并且内部有多个IEEE n节点的电力系统模型(The new Matpower 5.01 toolbox, can flow, optimal power flow, the time domain simulation and a series of calculation. Function is very powerful, and the internal power systems with multiple IEEE N node model)
- 2014-09-09 09:59:22下载
- 积分:1
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autoit-v3
自动化程序生成包,对于进行的操作编码和分析操作指令,生成可以重复使用的程序代码(Automatic program generation package for the operation code and the analysis operation instruction to generate the program code can be reused)
- 2014-11-06 09:07:14下载
- 积分:1
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0618fa
0.618法是根据黄金分割原理设计的,所以又称之为黄金分割法。 优选法是一种求最优化问题的方法。(0.618 method is designed based on the principle of golden, it is also called the golden section method. Optimization is an optimization problem seeking.)
- 2011-01-17 21:20:02下载
- 积分:1
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orbit
编程仿真连续小推力实现GTO到GEO的三阶段转移过程,其中推力器的推力大小为0.8N,轨道机动的起始点为GTO的远地点。GTO轨道的升交点赤经为0度,近地点角距为90度。
GTO轨道: ph:185km,ah:35786km,i:28.5°,GEO轨道:h:35786km,i:0°。
卫星质量为6600kg,从GTO到GEO,采用5000s的推力器。取地球半径为6378km,g取值为9.8m/s^2(The three stage transfer process from GTO to GEO is realized by simulation and continuous small thrust. The thrust of the thruster is 0.8N, and the starting point of orbital maneuver is the apogee of GTO. GTO orbit RAAN is 0 degrees, 90 degrees for the argument of perigee.
GTO orbit: ph:185km, ah:35786km, i:28.5, GEO orbit: h:35786km, i:0.
The mass of the satellite is 6600kg, from GTO to GEO, using the 5000S thruster. The radius of the earth is 6378km, and the value of G is 9.8m/s^2)
- 2021-01-28 10:38:35下载
- 积分:1
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Huffman3
MATLAB实现霍夫曼编码对英文文本的解压缩程序(MATLAB Huffman coding for the English version of decompression procedures)
- 2006-06-08 12:16:28下载
- 积分:1