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DATA16M

于 2008-07-18 发布 文件大小:4KB
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下载积分: 1 下载次数: 111

代码说明:

  这是在MATLAB环境下进行电力系统暂态稳定分析的pst源程序,该文件定义了一个16机的系统模型。(This is the MATLAB environment in power system transient stability analysis of the pst source, the document defines a 16-machine system model.)

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  • xinanjiangmoxing
    可直接用于新安江模型计算,修改输入模型文件即可。(Xin)
    2021-04-02 11:39:07下载
    积分:1
  • ED
    说明:  电力系统考虑网损的经济调度程序,采用的是经典算例,算例实用性较好。(Net loss of power system considering the economic dispatch procedures used are the classic example, a good practical example.)
    2009-03-12 10:03:40下载
    积分:1
  • qcgz
    Php使用技巧集 文件格式 chm 文件大小:61K()
    2017-10-10 08:12:10下载
    积分:1
  • zishiyingguangxuefangzheng
    自适应光学应用的一篇文章,可用于大气湍流和远距离观察时参考!(Adaptive optics applied to an article, can be used for reference atmospheric turbulence and remote viewing!)
    2015-10-04 14:46:10下载
    积分:1
  • EOAA
    现在很好用的一个BBS哦 是ACCESS的()
    2018-05-30 06:29:06下载
    积分:1
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    本软件进行了连续潮流法的改进,提高了连续潮流法的计算速度和收敛性,并利用改进后的方法对电力系统的电压稳定性进行了分析。(This software has been improved by continuous power flow method, which improves the calculation speed and convergence of the continuous power flow method, and the voltage stability of power system is analyzed by the improved method.)
    2016-11-07 15:41:48下载
    积分:1
  • 2649
    matlab code for fuzzy logic algorithm
    2010-11-18 02:15:42下载
    积分:1
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    Inverse kinematics algorithm for Robot position control. Based on end chapter problems in Sciciliano et al book for Robot motion control. Different methods are used and their results provided.
    2021-03-19 13:49:19下载
    积分:1
  • cal_class
    说明:  ;Method : 0-平行六面体 ; 1-最小距离 ; 2-最大似然 ; 3-马氏距离 ; 4-神经元网络 ENVI_NEURAL_NET_DOIT ; 5-向量机 ENVI_SVM_DOIT ; 6-IsoData ; 7-K-Means(method: 0-parallelepiped 1 - minimum distance 2-maximum likelihood 3-mahalanobis distance 4-neural network 5-vector machine envi? SVM? Doit 6-IsoData 7-K-Means)
    2020-02-27 11:20:51下载
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  • C-W
    使用CW方程,使用最小能量,采用脉冲推力,实现在一天内两航天器的交会对接。本质上就是一个交会轨道优化问题,由给定的条件优化选取设计变量,使目标函数得到最优值。(Using the CW equation, use the minimum energy, the use of pulse thrust, to achieve in a day two spacecraft rendezvous and docking. Is essentially an intersection orbit optimization problem, by the given conditions to optimize the selection of design variables, so that the objective function to get the optimal value.)
    2017-05-11 20:05:29下载
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