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MATLAB_2
主要内容：
概述
创建向量
创建矩阵
向量和矩阵元素的索引（重点）
向量和矩阵的基本操作 （重点）
多维数组
(failed to translate)
- 2009-04-05 21:38:38下载
- 积分：1
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texture-analysis
基于熵的纹理分析，我目前用来做海面上的油斑检测(Entropy-based texture analysis, I present the oil used to make spot inspection on the sea)
- 2011-01-26 05:11:30下载
- 积分：1
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DSPmatlab
说明： Dsp中的Matlab ，
AFD_BUTT.M AFD_CHB1.M AFD_CHB2.M(Dsp of Matlab, AFD_BUTT.M AFD_CHB1.M AFD_CHB2.M)
- 2006-04-27 19:59:25下载
- 积分：1
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The-most-practical-matlab-code
matlab最实用代码matlab最实用代码matlab最实用代码(The most practical matlab code code matlab matlab most useful code in the most practical)
- 2011-12-28 17:32:34下载
- 积分：1
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parabolic_PDE_1_2D_explicit
explicit FDM for 1_2D_parabolic partial differential equation
- 2014-02-07 16:11:26下载
- 积分：1
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ff
说明： 本程序是数字图像矩阵数据的显示及其傅立叶变换的应用(digital image data matrix display and the application of the Fourier transform)
- 2006-05-25 15:14:21下载
- 积分：1
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SlidingControToChaos
采用滑模控制对LORENZE混沌系统进行抑制(Sliding Control To Lorenze Chaos system)
- 2020-12-05 14:09:22下载
- 积分：1
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Madaline
Madaline Neural Network for character recognition. Designing a Madaline (Multiple Adaline) Neural Network to recognize 3 characters 0, C and F supplied in a binary format and represented using a 7x7 grid. The Neural Network should be trained and tested with various patterns, then the total error rate and the amount of convergence should be observed.
- 2013-11-05 04:50:19下载
- 积分：1
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73
说明： 是一本不可多得的仿真书籍，5个文件为该书随书附带源代码(Simulation is a rare books, 5 source code files for the book that came with the book)
- 2012-11-16 14:35:52下载
- 积分：1
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Reconfigurable-flight-control
精密控制结构需要满足先进飞机的使命和对其引航的要求。这就要求飞行器的性能必须满足在低空飞行，低速飞行和大迎角攻击性飞行，全天候，昼夜工作的条件，并且新的控制技术应该成熟。这项工作提出了飞行控制时，状态变量和控制输入是由预先确定的限制范围内的系统控制系统的设计理念。在设计过程使用动态规划的概念。其基本思想涉及非二次泛函最小化。由于一系列限制因素，建议使用光滑函数。同时提出了该综合方法的优点。我们利用对F-18战斗机的纵向控制配置来说明该设计方法。(Indirect adaptive control for reconfigurable flight control is advocated. Specifically,
online static system identification using a moving window/batch estimation is implemented.
The ensuing linear regression is augmented with an intercept. The intercept parameter is
included to address the effects of trim change associated with the occurrence of a control surface
failure. Parameter estimate information is used to adjust the inner loop’s control gains, and
a command derived from the intercept estimate is fed forward to automatically retrim the aircraft.
The tracking performance of this automatic retrimming method, which relies on system
identification, surpasses the conventional approach of exclusively relying on integral action
for retrimming. These adaptive and reconfigurable flight control concepts are illustrated in
the context of a fighter aircraft’s pitch plane dynamics. The novel adaptive and reconfigurable
flight control system successfully handles a 50 per cent horiz)
- 2011-05-02 12:39:11下载
- 积分：1
