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LMI_example
线性矩阵不等式的完整程序，对初学者来说是不错的资料，快下载吧。(LMI complete program for beginners is good information, fast to download it.)
- 2011-04-30 10:36:24下载
- 积分：1
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dimension_full
matlab mfile for chaos
- 2012-06-14 16:30:14下载
- 积分：1
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Arnold000
说明： 这是一个混沌的Anrold变换 他是一次变换加密 是一个混沌加密入门程序(This is a chaotic Anrold transform He is a transformation encryption is a chaotic encryption entry procedures)
- 2021-03-03 15:39:33下载
- 积分：1
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Bilinear-transformation-method
设计低通数字滤波器，要求在通带内频带低于 时，允许幅度误差在1dB以内(Design of digital low pass filter, requirements in the passband frequencies below, allow a margin of error of less than 1dB,)
- 2012-04-20 17:23:43下载
- 积分：1
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compare_segmentations
This is very important code for image segmentation comparisons, this code calculates RI, GCE and VI for segmentation comparisons.
- 2013-09-22 20:11:33下载
- 积分：1
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pangbanduixiao
雷达旁瓣对消器，应用于雷达抗有源旁瓣干扰。(Radar sidelobe canceller, used anti-active radar sidelobe interference.)
- 2021-01-25 19:38:38下载
- 积分：1
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eebmcfnb
通过matlab编写的deVOrNH程序。Mallat变换以及小波变换在边缘提取、图像去噪、数据压缩等中的应用，特别包含了二代提升小波的相关内容，理论与实际相结合。大家想要了解的二进小波、正交镜像滤波器组[qqWxzjW]等概念这里都有体现。(By MATLAB program deVOrNH, Mallat transform and wavelet transform in edge extraction, image denoising, data compression, etc. in the application, especially includes the second generation wavelet related content, theory and practice. We want to understand the two into the wavelet, the quadrature mirror filter bank [qqWxzjW] and other concepts here are reflected.)
- 2016-02-16 18:56:10下载
- 积分：1
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hilbert-for-radar-signal-processing
用希尔波特分析分析雷达信号细微特征法的分析方法特点(Hilbert analysis with analysis of radar signal analysis method is characterized by subtle features)
- 2016-04-07 16:34:45下载
- 积分：1
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月球软着陆程序
说明： 月球软着陆仿真：在停泊轨道上，探测器在脉冲制动的作用下，经霍曼变轨，下降到距月面大约 15 公里的近月点，该近月点就是主制动段的初始制动点。主制动段以下是障碍检测与规避和最终着陆段。在主制动段，由于探测器的初始速度很大(1.692km/s)，所以主制动段制导律设计的主要目的就是高效抵消此速度，将探测器导引到期望的末端状态(Lunar soft landing simulation: in the parking orbit, the probe under the action of pulse braking, through the hohmann change of orbit, to descend to about 15 kilometers from the surface of the moon, the near-moon point is the main braking section of the initial braking point. Following is the main braking section for obstacle detection and avoidance and the final landing section. In the main braking section, since the initial velocity of the detector is very large (1.692km/s), the main purpose of the guidance law design of the main braking section is to effectively offset this velocity and guide the detector to the desired terminal state)
- 2021-01-28 22:18:35下载
- 积分：1
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dace
说明： 克里金代理模型的DACE工具箱，可用于优化计算(The dace toolbox of Kriging agent model can be used for optimization calculation)
- 2020-10-11 16:03:20下载
- 积分：1
