登录
首页 » matlab » MUSIC

MUSIC

于 2011-08-15 发布 文件大小:1KB
0 276
下载积分: 1 下载次数: 3

代码说明:

  经典的MUSIC算法,使用MAtlab编程实现(Classic MUSIC algorithm)

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

  • matlab
    matlab 教程 简明的matlab的ppt经典教程 (matlab tutorials matlab concise tutorial in ppt Classic)
    2010-01-20 14:13:57下载
    积分:1
  • Convulutional_Encode_Viterbi_Decode
    Encoded by Systematic convolutional code, decoded by Viterbi using Hamming distance.
    2009-07-14 14:31:58下载
    积分:1
  • Engineering-Optics-With-Matlab
    介绍了Matlab在光学仿真中的应用,包括了几何光学、光波导、高斯光束传输等方面的基础知识及仿真。(Engineering Optics With Matlab)
    2011-12-27 11:31:08下载
    积分:1
  • pCOST207
    Matlab code for COST207 channel
    2009-10-09 07:39:38下载
    积分:1
  • newtonmethod
    用matlab编写的牛顿迭代方法求解非线性方程组:数值分析中很经典的代码(a matlab code of newton method solve system of nonlinear equations)
    2014-01-29 20:24:22下载
    积分:1
  • optimization_of_dexterous_hand
    优化灵巧手的各节长度,适用于多指灵巧手的手指结构优化设计的多目标优化函数。(to optimize the length of finger)
    2009-04-15 17:41:06下载
    积分:1
  • erle
    可以用来测量线路回声消除效果的matlab程序(lines can be used to measure the effects of echo cancellation procedures Matlab)
    2021-04-16 10:38:53下载
    积分:1
  • matlab
    包含一些通信系统的仿真程序 包括时间分集,频率分集,二时二频分集(Communication system contains some simulation program including time diversity, frequency diversity, frequency diversity two two)
    2013-11-27 14:20:44下载
    积分:1
  • mont-carlo-tsp
    tsp with mont carlo algorithm
    2011-05-01 14:23:01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
  • 696516资源总数
  • 106914会员总数
  • 0今日下载