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control2
online identification using neural network
- 2015-02-10 04:30:55下载
- 积分:1
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4
说明: 实验4 基于MATLAB的数字滤波器设计 有效的设计IIR和FIR滤波器(Experiment 4 MATLAB-based digital filter design effective design IIR and FIR filters)
- 2010-08-14 22:04:28下载
- 积分:1
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p3
说明: image processing and noise models
- 2010-11-22 04:45:50下载
- 积分:1
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kMeansCluster
说明: K-均值聚类,比较好的聚类方法,应用广泛(K-means clustering, a better clustering method, widely used)
- 2008-11-17 16:16:38下载
- 积分:1
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EMD-decomposition-programe
Hilbert-Huang变换之EMD分解程序。可以直接运行,以及附有几个详细例子。可以用以对非线性非平稳信号的处理,效果理想。(Hilbert-Huang transform EMD decomposition process. Can be run directly, as well as with several detailed examples. Can be used for non-linear non-stationary signal processing, the results are satisfactory.)
- 2013-05-12 21:38:41下载
- 积分:1
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FH-simulation
By using this matcode codes a simple frequency Hopping system can be simulated. The number of frequencies to be used can be changed by changing the parameters
- 2014-02-20 19:26:34下载
- 积分:1
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MPSK_SIM_4
MPSK simulation
1. System Parameters
2. Data Generation
3. Modulation
4. AWGN
5. Demodulation
6. Detection
- 2011-05-16 23:36:39下载
- 积分:1
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pseudo-random-code
仿真实现了伪随机码的产生过程,包括m序列,C/A码以及金码等(simulation of pseudo-random code)
- 2011-08-27 14:31:52下载
- 积分:1
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SparseOLS
implementation ols sparse algorithm
- 2013-10-23 22:39:27下载
- 积分:1
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Wind-turbine-blades-design
本文利用MATLAB的遗传算法工具箱,对弦长和扭角沿风力机展向分布进行优化,得到设计工况下的最优叶片设计。目标函数是设计工况下基于动量叶素理论和Glauert等修正所得出的功率系数。在设计工况下得到的设计结果,其功率系数在一定的风速范围内都能保持一个较高的数值,同时其有效攻角分布大致都在所选翼型的升力与阻力系数的比值最大处,与理论相符合。其结果说明该优化实际的有效性。(In this paper, the use of MATLAB genetic algorithm toolbox, chord length and twist angle along the wind turbine development to distribution optimized to obtain the optimal design conditions blade design. The objective function is to design conditions based on the results of momentum blade element theory and Glauert correction power factor. Design results in the design conditions, the power factor within the range of wind speeds can maintain a higher value, the effective angle of attack distribution substantially in the the selected airfoil lift and drag coefficient ratio of maximum , theoretical analysis and show. The results indicate the validity of the actual optimization.)
- 2013-04-21 14:06:41下载
- 积分:1