登录
首页 » matlab » AD1

AD1

于 2012-04-13 发布 文件大小:1KB
0 252
下载积分: 1 下载次数: 54

代码说明:

  利用复自相关法求取混沌时间序列的时间延迟(tau),求取算法效率高且准确(Complex strike a chaotic time series autocorrelation time delay (tau), to strike a high efficiency of the algorithm and accurate)

文件列表:

下载说明:请别用迅雷下载,失败请重下,重下不扣分!

发表评论

0 个回复

  • Gabor_2dpca_pca
    指纹识别系统设计全过程实现 matlab软件环境实现(Fingerprint identification system the entire process of design implementation software environment implementation matlab)
    2009-03-28 11:43:55下载
    积分:1
  • stochasticResonance
    随机共振作出SNR信噪比随噪声强度变化的曲线(matlab code for stochastic resonance!used for plotting the figure about SNR versus D(noise strength))
    2020-12-03 23:09:24下载
    积分:1
  • mohsins
    tasks of matlab in seecs
    2010-11-09 21:11:26下载
    积分:1
  • 2
    说明:  滑膜变结构控制的matlab仿真程序,学习滑膜变结构控制的基础。(Variable structure control synovial matlab simulation program, learning the basis of variable structure control synovium.)
    2011-04-17 18:48:35下载
    积分:1
  • PSO
    基于粒子群的神经网络优化算法的应用,在土壤水分特征曲线中的应用。(Neural network based on particle swarm optimization algorithm applied in the soil moisture characteristic curve application.)
    2013-10-18 13:44:10下载
    积分:1
  • pscad_4_2_veterna_elektraren
    model of wind power plant with synchronous generator, created in pscad 4.2
    2015-01-23 22:26:31下载
    积分:1
  • huiguifenxi
    这是数学算法中的回归分析法 联合开发网 - pudn.com
    2012-04-17 19:11:36下载
    积分:1
  • sgwt_toolbox
    谱图理论的MATLAB相关编码和相关的源程序(MATLAB spectral theory associated source code and related)
    2020-12-02 16:59:26下载
    积分:1
  • KALMAN
    Kalman filter simulation on Matlab code
    2010-11-19 11:53:03下载
    积分:1
  • 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
  • 696516资源总数
  • 106914会员总数
  • 0今日下载