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BeeColony
Matlab Implementation of Population based Global Bee Colony Search Algorithm
- 2009-03-21 03:26:41下载
- 积分：1
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cor_embed
image watermarking method
- 2011-06-13 18:22:52下载
- 积分：1
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Ex6_pmm
example simulation s of analysis of electrical machinery and drive systems - Pual C. Krause - Ex6
- 2013-10-04 04:31:13下载
- 积分：1
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肌电信号高低滤波与陷波器算法
肌电信号高低滤波算法与50Hz陷波器算法，仿真已通过(The EMG high-low filter algorithm and 50Hz notch filter algorithm have been simulated.)
- 2019-02-25 18:31:08下载
- 积分：1
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utxdgfxn
滤波求和方式实现宽带波束形成，基于分段非线性权重值的Pso算法，这个有中文注释，看得明白，通过matlab代码，非归零型差分相位调制信号建模与仿真分析 ，matlab程序运行时导入数据文件作为输入参数，使用拉亚普诺夫指数的公式，抑制载波型差分相位调制。( Filtering summation way broadband beamforming, Based on piecewise nonlinear weight value Pso algorithm, The Chinese have a comment, understand it, By matlab code, NRZ type differential phase modulation signal modeling and simulation analysis, Import data files as input parameters matlab program is running, Raya Punuo Fu index using the formula, Suppressed carrier type differential phase modulation.)
- 2016-04-06 22:10:55下载
- 积分：1
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342225144NoisenewTVInpaintingTest
说明： 基于TV模型的图像快速修复自适应方法，欢迎大家分享(TV model based on adaptive methods of image quick fix, please share)
- 2011-04-11 15:31:34下载
- 积分：1
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Matlab_Radar_Simulation
一个编写的地面雷达的MATLAB仿真程序，基本包括了雷达的各项功能，适合初学者对雷达原理的了解和认识(A preparation of ground radar MATLAB simulation program, basically covers the various functions of the radar, the radar for beginners knowledge and understanding of the principles of)
- 2013-08-20 20:21:51下载
- 积分：1
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fxlms_with_sine_input
FXLMS algorithm with sign wave as a input matlab program adaptive algo.
- 2013-04-26 19:20:33下载
- 积分：1
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基于二阶统计量与四阶通计量的时延估计算法 tde
基于二阶统计量与四阶通计量的时延估计算法。(Delay estimation algorithm with second-order and fourth-order statistics.)
- 2014-08-28 21:36:22下载
- 积分：1
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han1
这里我们针对三级固体火箭进行研究，主要考虑每一级发动机工作时推力 和比冲 与发动机试车存在摄动偏差（相差 ）时所产生火箭关机点时刻的状态偏差。火箭的飞行的动力学方程可建立在地面发射坐标系中，火箭的第一级、第二级和第三级按照固定的俯仰角程序飞行，第二、三级飞行时已在大气层外，此时可忽略气动力的影响。(Here we study for three solid rocket, the main consideration at every level when the engine thrust and state arising the moment the rocket off point perturbation deviation (difference) in the presence of specific impulse and engine test bias. Outside of the rocket flight dynamics equations can be established on the ground coordinate system launch, the rocket s first stage, the second and third stages according to a fixed elevation angle of flight procedures, and the second, when the third flight already in the atmosphere, this when can ignore the effects of gas dynamics.)
- 2020-11-03 20:39:53下载
- 积分：1
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