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HysteresisSVPWM03
SVPWM的实现,调试通过.对输入波形的跟踪非常精确,THD小于0.2 .本来作为APF中替代滞环比较用的.(SVPWM implementation, debugging through. On the input waveform of the tracking is very accurate, THD less than 0.2 . Have been replaced as the APF Hysteresis in use.)
- 2010-09-08 13:41:47下载
- 积分:1
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9879878978907890
该文档描述了NP0等电容的性能参数与规格。(NP0 capacitor such as described performance parameters and specifications.)
- 2010-12-05 08:43:24下载
- 积分:1
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intromat
Introduction à
MATLAB et Simulink
- 2010-06-28 18:45:28下载
- 积分:1
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targil3
m-pskmodulation and de modulation
- 2010-09-08 01:31:33下载
- 积分:1
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feedbackkfilter
反馈试滤波器设计 在图像处理和滤波器设计方面有非常广泛的引用 matlab 程序 付仿真(feedback matlab code)
- 2010-09-27 17:38:26下载
- 积分:1
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TDOATaylorAlgorithm
TDOA定位算法,用于实现无线定位中的TAYLOR算法(TDOA location algorithm for wireless location algorithm TAYLOR)
- 2014-01-10 02:59:30下载
- 积分:1
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frequencycoefficients
将图像分为nxn的分块,之后将各分块三个颜色通道的直方图平均化,最后进行离散余弦变化,分别提取各通道低频系数(The image into nxn sub-block after block of all three color channels of the histogram equalization, and finally the discrete cosine change, were extracted from the low frequency coefficients of each channel)
- 2010-11-21 19:00:16下载
- 积分:1
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matlabparticle
基于粒子滤波实现的目标被动跟踪,适合初学者学习。(Goal-based particle filter tracking, suitable for beginners to learn.)
- 2010-05-11 20:53:54下载
- 积分:1
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03041507
在某初教机的线性模型基础上,建立了飞机的纵向和横向传递函数,分析了模型参数的不确定性,通过使用MATLAB中的NCD模块对飞行控制系统及PID控制器等参数进行优化,设计出了飞机的自动驾驶仪高度保持和航向保持模式。这种方法既避免了复杂的计算和编程,又使系统具有较好的稳定,陛、动态性能和鲁棒性,克服了飞机模型参数随着高度和速度的变化(即模型参数存在不确定性)而需要按照多个不同高度和速度的飞行区域设计一系列控制器的缺点(early in a plane of the linear model, based on the aircraft's vertical and horizontal transfer function, Analysis of the model parameters of uncertainty, MATLAB through the use of the NCD Blocks flight control system and PID controller parameters for optimization, design of the aircraft's automatic pilot systems, and maintain a high degree course-keeping mode. This method not only avoids the complex calculation and programming, the system has good stability, Her Majesty, dynamic performance and robustness. overcome the aircraft model parameters with the height and speed of change (that model parameters uncertainty exists) and the need to not more than with the height and speed of regional flight controller design a series of shortcomings)
- 2007-05-12 09:58:13下载
- 积分:1
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table-for-sin-functionof-
DDS中的正余弦生成,初始相位相差90度,可自行改变输出频率(Cosine generation of DDS, the initial phase difference of 90 degrees, the output frequency can be changed on their own)
- 2013-12-17 22:09:56下载
- 积分:1