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自方幂数问题
说明: matlab,对解决学习中遇到的实际问题会有很大的帮助(Matlab, learning to solve practical problems encountered in will be a big help)
- 2005-12-08 14:14:17下载
- 积分:1
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FINDFILE
Recursive File Search
Purpose: Traversal across an entire hard drive
The SearchForFile function should work in any program provided you include the PROTO
below.
Note: This is a console mode program and builds with Project|Console Assemble & Link
- 2014-02-18 20:21:14下载
- 积分:1
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MATLAB/Simulink模型 SOH-Folder
一个MATLAB/Simulink模型,关于电动汽车动力电池健康状态(State of Health;
建模基于SOC估计;
模型比较简单,原理清楚,适合对电动汽车动力电池SOH的估计有兴趣的初学者参考学习,学习前请阅读2到3篇动力电池SOH估计方面论文,这样对理解模型更有帮助。(A MATLAB/Simulink model, on the electric vehicle power battery health status (State of Health
Modeling based on SOC estimation
Model is relatively simple, the principle is clear, suitable for beginners interested in electric vehicle power battery SOH estimation, it will be better to read 2 to 3 SOC estimation papers about battery SOH estimates.)
- 2021-04-27 11:08:45下载
- 积分:1
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rengongyiqunsuanfa-matlab
人工智能算法,蚁群算法,人工免疫算法等matlab程序(Artificial intelligence algorithms, ant colony algorithm, artificial immune algorithm matlab program)
- 2013-01-02 21:19:17下载
- 积分:1
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shuzixinhaochuli_daan
digital signal processing solution
- 2014-09-30 16:08:23下载
- 积分:1
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osdef1st
The information in this file is provided AS IS without warranty.
- 2014-10-13 13:59:05下载
- 积分:1
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weifeng
对于风荷载用matlab进行编程计算分析代码(Computational analysis for wind loads using matlab programming)
- 2013-03-17 21:21:55下载
- 积分:1
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matlabbpnn
基于matlab的三层bp神经网络源程序代码(based on the three-tier bp Matlab neural network source code)
- 2006-09-23 22:45:36下载
- 积分:1
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ganshe
该程序可以让你通过设置一序列参数来获得具有一定距离的两波源实现干涉(This program lets you set up a sequence of parameters through to get some distance the two wave source to achieve interference)
- 2015-04-02 21:05:53下载
- 积分:1
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LanderMission
这个课题设计从地球的近地轨道起飞到达谷神星预定轨道并且着陆在其表面上的一种数值方法。基于有限时间的航行纠正点火而非瞬时推力数值计算和Matlab仿真。最后可以看到空间飞行器从地球的影响球飞到谷神星的影响球的飞行轨迹。(This project explores the mathematical methods and results of designing a mission to land a spacecraft on the asteroid Ceres by beginning in an earth-centered LEO orbit and ending in an orbit prepared to land on the surface of the asteroid. Rather than assume instantaneous velocity changes, course-correcting burns of finite time are considered and analyzed using numerical methods and Matlab computation. The behavior of the spacecraft is observed inside the Earth s sphere of influence, in interplanetary space, and inside Ceres sphere of influence. )
- 2010-01-12 13:42:02下载
- 积分:1