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growcut
growcut algorithm is implemented for segmentation purpose
- 2013-09-19 17:52:08下载
- 积分：1
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[ebook]-DSP---Introduction-to-Signal-Processing-(
[ebook] DSP - Introduction to Signal Processing (code in C & MatLab)
- 2014-01-22 00:38:30下载
- 积分：1
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GA_ex
Genetic Algorithm Matlab code with 3 exaples
- 2015-04-17 16:46:46下载
- 积分：1
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random_walker_matlab_code
The random walker algorithm was introduced in the paper:
Leo Grady and Gareth Funka-Lea, "Multi-Label Image Segmentation for Medical Applications Based on Graph-Theoretic Electrical Potentials", in Proceedings of the 8th ECCV04, Workshop on Computer Vision Approaches to Medical Image Analysis and Mathematical Methods in Biomedical Image Analysis, p. 230-245, May 15th, 2004, Prague, Czech Republic, Springer-Verlag.
Available at: http://cns.bu.edu/~lgrady/grady2004multilabel.pdf
- 2010-05-06 01:50:32下载
- 积分：1
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sign
matlab中用户自编的几个非常常用的函数集结，适合初学者(matlab users own several very commonly used function of the assembly, suitable for beginners)
- 2008-03-04 20:10:30下载
- 积分：1
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Filterdesign
matlab重要的学习资料 初学者的好帮手 程序代码非常重要(matlab important information for beginners to learn a good helper program code is very important)
- 2010-10-06 19:48:42下载
- 积分：1
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fehrs1
Das Tagebuch von Fehrs
- 2010-11-23 02:20:28下载
- 积分：1
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shang
此段程序为matlab程序，用熵值法计算城市化综合指数(shang method to calculate urbanization composite index)
- 2013-03-06 09:44:59下载
- 积分：1
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matlab
说明： 较为详细和全面的介绍了MATLAB在仿真系统中应用。(More detailed and comprehensive introduction to the MATLAB application in the simulation system.)
- 2010-04-08 19:26:03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
