登录
首页 » matlab » f_path

f_path

于 2011-10-10 发布 文件大小:1KB
0 86
下载积分: 1 下载次数: 22

代码说明:

  图论及复杂网络中,Warshall-Floyd算法求解两点间最短路径。(Figure dealt with complex networks, Warshall-Floyd algorithm to solve the shortest path between two points.)

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

  • Frank_gen_new
    用于产生Frank多相编码复数序列,然后将得到的编码做相关(generate code and make it throngh matched filter)
    2010-10-22 15:52:26下载
    积分:1
  • sl_using
    Simulink. Dynamic System Simulation for MATLAB. aka "Using Simulink". This is the book about Modeling, Simulation and Implementation with Simulink package.
    2010-11-06 01:01:24下载
    积分:1
  • 113
    说明:  利用Matlab引擎、利用Matlab编译器、利用Matcom软件编译、调用Matlab数学函数库、及调用Matcom数学函数库。(Using Matlab engine, using Matlab compiler, use Matcom software build, call Matlab math library, and calls Matcom math library.)
    2010-03-31 20:39:37下载
    积分:1
  • ImageCompression
    图像进行小波分解后,对于相对来说不重要的高频成份采用较高的阈值,进行高压缩;而对集中图像大部分能量的低频成分采用较小阈值,以确保图像恢复时的质量(Image Compression)
    2009-06-06 23:23:22下载
    积分:1
  • 1.2-Mutual_Info
    Matlab and C code of mutual information
    2015-03-16 15:57:45下载
    积分:1
  • flt_calc
    filter calculations matlab files
    2010-06-13 17:37:49下载
    积分:1
  • Neuralnetworktoolbox
    Matlab神经网络工具箱的应用简介,从原理到应用(Neural network toolbox)
    2010-01-18 22:08:49下载
    积分:1
  • 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
  • NoncoherentAGC
    Coherent Reception of BPSK transmission
    2010-06-28 23:14:17下载
    积分:1
  • FFTinGUI1
    This program makes the out put to the serial output port
    2009-05-07 19:22:16下载
    积分:1
  • 696518资源总数
  • 104432会员总数
  • 16今日下载