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final1DFIG
doubly fed reluctance generator based wind energy conversion system
- 2012-07-15 19:08:58下载
- 积分：1
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3
信号处理,进行信号检测与处理，通过设定threshold来进行信号检测的可信度调整(Credibility adjustment signal processing, signal detection and processing, by setting threshold for signal detection)
- 2013-12-02 04:18:11下载
- 积分：1
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Turbo-and-Ldpc
Turbo与LDPC编解码及其应用（肖扬）书中程序(Turbo and LDPC encoding and decoding and application program (Xiao Yang) in the book)
- 2021-03-20 21:49:18下载
- 积分：1
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lowpass_IIR
低通IIR滤波器的源码，简单有效。低通IIR滤波器的源码，简单有效(Low-pass IIR filter source, simple and effective. Low-pass IIR filter source, simple and effective)
- 2010-06-18 17:08:54下载
- 积分：1
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1
说明： 一些自己编写的图像插值算法程序。包括最近邻插值，双线性插值和双三次插值(-Recently, the field of bilinear interpolation and interpolation matlab source, comparing the effects of two algorithms.)
- 2012-05-01 13:52:55下载
- 积分：1
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mfc
matlab for MICROSOFT FOUNDATION CLASS LIBRARY
- 2014-12-19 08:56:10下载
- 积分：1
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Survey
生成纵横向四阶方程，计算特征根，传递函数等，给出波特图及尼科尔斯图。( SURVEY is set up to make calculations based on the 12 x 12 Fmodel and 12 x 7 Gmodel produced by FLIGHT, with the generic business jet model trimmed for flight at V = 102 m/s and h = 3,050 m. The flags are set to generate a fourth-order, body-axis, lateral-directional model the data set to calculate eigenvalues, eigenvectors, and the transfer function aileron to roll rate and to show the Bode plot, Nyquist plot, and Nichols chart for the transfer function.)
- 2015-10-17 22:45:30下载
- 积分：1
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reynoldswending
解析法建立挤压油膜阻尼器稳态数学模型并仿真特性关系(Analytical method SFD to establish steady-state characteristics of the mathematical model and simulation relations)
- 2009-04-26 17:10:32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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speechdetect
It is a matlab file performing Speech detection
- 2012-05-28 20:13:14下载
- 积分：1
