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the-braking-curve
用matlab绘制的车辆制动曲线，以起亚K9为参考模型，用的时候改下参数即可(Matlab mapping the vehicle braking curve, the Kia K9 as a reference model, when used to change the parameters can be)
- 2012-05-03 07:05:26下载
- 积分：1
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invMarguarotWem
线性反演方法中的马夸特反演算法 matlab程序(Linear inversion method of Marquardt inversion algorithm matlab program)
- 2012-05-25 09:22:48下载
- 积分：1
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matlab-fft
基于matlab的地震傅式谱编写程序，很有用的一个程序。(Fuh-based seismic spectrum matlab programming, a very useful program.)
- 2013-09-26 19:16:56下载
- 积分：1
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Untitled
三次样条曲线插值函数的matlab源程序(three spline curvs)
- 2011-05-26 13:13:57下载
- 积分：1
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fick2
扩散的菲克第二定律的数值求解
第一次弄，请大家赐较(Colorific proliferation of the second law of the numerical solution of the first alley, please grant more)
- 2020-06-28 20:20:02下载
- 积分：1
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radar
内容为 自适应复高斯雷达目标识别 的Matlab程序。
(Content adaptive reuse Gaussian radar target recognition Matlab procedures.)
- 2014-01-27 17:33:56下载
- 积分：1
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Matlab2010
matlab 初学者书籍，对初学者有很大的帮助(matlab beginner books, there is a great help for beginners)
- 2015-04-17 20:42:21下载
- 积分：1
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matlab-code-for-wimax
WiMax physical layer MATLAB code
- 2011-10-16 18:44:41下载
- 积分：1
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R_N_U
原理：乘同余法产生随机数来生成均匀分布、瑞利分布、正态分布，压缩包包括3个分布的Matlab源代码(Principle: multiplicative congruential method to generate random numbers to generate uniformly distributed ，Rayleigh distribution and normal distribution.This package includes three distribution of Matlab source code.)
- 2013-11-02 14:24:01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
