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lude2
Matlab file for Part 2 of the LU Decomposition module
- 2011-03-18 12:42:58下载
- 积分：1
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Bezier-cures
本文研究了三次bezier曲线与三次B样条曲线的光滑拼接，用matlab可以实现这个过程(This paper studies the three bezier curves and cubic B-spline curves and smooth stitching, this process can be achieved using matlab)
- 2013-05-19 02:53:24下载
- 积分：1
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FaultyPolar
改进的polar码解码算法faulty sc decoder，及其matlab实现(the improved sc decoding algorithm named faulty sc decoder, and its implementation in matlab)
- 2020-11-28 20:39:28下载
- 积分：1
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cvery_20528401
说明： 在matlab中，以simulink为主要工具介绍了系统仿真方法与技巧，包括连续系统、离散系统、随机输入系统和负数系统的仿真。(In matlab in order to simulink introduced as the main tool for system simulation methods and techniques, including continuous systems, discrete systems, stochastic systems and the negative input of the simulation system.)
- 2008-10-22 21:55:23下载
- 积分：1
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dace
这个程序纪要是用于克里金差值拟合的dace调用，dace程序简化了克里金调用(The summary of this program is the dace call for the Kriging difference fitting. The dace program simplified the Kriging call.)
- 2018-05-09 22:31:26下载
- 积分：1
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Polynomial Regression
多项式回归代理模型的相关程序及算例，可选择线性、二阶、三阶多项式进行计算(The related procedures and examples of the polynomial regression proxy model can be selected by linear, second-order and third-order polynomials.)
- 2020-11-02 17:09:54下载
- 积分：1
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hurst指数
说明： 里面包含可运行的栅格数据，m文件，加载m文件即可运行(It contains data code)
- 2020-06-06 21:31:50下载
- 积分：1
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LingoLindo
Lingo,lindo与数学建模，主要讲述lingo,lindo在数学建模中的应用以及一些关于lingo和lindo的函数等知识。(Lingo, lindo and mathematical modeling, primarily on the lingo, lindo in the Mathematical Modeling as well as some on the lingo and knowledge lindo function.)
- 2007-08-26 21:02:36下载
- 积分：1
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v3d
matlab 三维显示。所有代码都有。可以显示三维网格。(three-dimensional display matlab. Have all the code. Can display three-dimensional grid.)
- 2009-04-21 09:35:08下载
- 积分：1
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Application
说明： 对弹丸飞行稳定性进行了分析,文中提出利用M GAERO 气动软件计算弹丸的气动力参数,以减少采
用经验公式估算气动力系数和压心位置等参数带来的误差,可为弹丸飞行稳定性分析和总体参数设计提供
参考依据。(For projectile flight stability analysis, this paper proposes the use of software to calculate projectile M GAERO aerodynamic aerodynamic parameters to reduce the use of empirical estimates of aerodynamic coefficients and parameters such as pressure center position error caused by, for projectile flight stability analysis and overall parameters of the design of reference.)
- 2010-03-16 19:08:49下载
- 积分：1
