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等高线拟合程序matlab
等高线拟合源代码(matlab源码),老外编的,水平确实可以,佩服。里面注释挺详细了。(contour fitting source code (Matlab source), a foreigner series, level really can admire. Inside Notes quite detailed.)
- 2020-11-18 11:49:38下载
- 积分:1
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滤波法
说明: A、名称:限幅滤波法(又称程序判断滤波法)
B、方法:
根据经验判断,确定两次采样允许的最大偏差值(设为A),
每次检测到新值时判断:
如果本次值与上次值之差A,则本次值无效,放弃本次值,用上次值代替本次值。
C、优点:
能有效克服因偶然因素引起的脉冲干扰。
D、缺点:
无法抑制那种周期性的干扰。
平滑度差。(A. Name: Limited filter method (also known as program judgement filter method)
B. Method:
Based on experience, the maximum allowable deviation (set to A) of two sampling times is determined.
Judge each time a new value is detected:
If the difference between the current value and the previous value is
- 2020-06-24 18:20:01下载
- 积分:1
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taup
t-p变换方法与应用,应用于地震资料处理中,是比较好的一本书(tp transform methods and applications used in seismic data processing is a good book)
- 2010-05-24 16:01:29下载
- 积分:1
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BPA
主要内容包
括:潮流数据格式说明,潮流数据,潮流结果。在尽可能的情况
下提供网络结构图,并提供数据的出处,以及我们对其潮流计算
和结果的一些感受。(power code)
- 2009-06-22 09:48:23下载
- 积分:1
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Synthetic-seismogram
运用雷克子波合成地震记录,可以根据自己需要更改模型参数。(Ricker wave using synthetic seismograms, you can change the model parameters according to their own needs.)
- 2014-04-07 16:47:54下载
- 积分:1
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model_build
对具有进动形式的空间目标进行微多普勒提取(Micro Doppler extraction of space target)
- 2021-04-21 10:28:49下载
- 积分:1
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选线仿真模型
小电流系统接地选线仿真模型及稳态零序功率方向法仿真算法(Simulation model of grounding fault location for small current system and simulation algorithm of steady zero sequence power direction method)
- 2018-05-10 19:38:32下载
- 积分:1
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GPS-SINS
GPS与惯性导航的组合导航,没有解释语句,但稍微有点基础一看就明白,(GPS and inertial navigation combination of navigation, did not explain the statement, but a bit on the basis of a look that)
- 2008-12-13 10:08:42下载
- 积分:1
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DATA3M9B
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3机9节点的系统模型。(This is the MATLAB environment in power system transient stability analysis of the pst source, the document defines a 3-machine 9-bus system model.)
- 2008-07-18 11:38:29下载
- 积分:1
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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
- 积分:1