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SimulinkModel
描述Matlab的Simulink的模型创建方法和仿真方法，是学习Simulink的好资料(This file is write for the Simulink of Matlab)
- 2010-06-29 10:46:38下载
- 积分：1
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1
说明： voicebox语音处理matlab工具箱【1】(VoiceBox voice processing toolbox matlab [1])
- 2008-05-31 12:11:23下载
- 积分：1
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sampling-and-reconstruction-code_matlab
1.Matlab code for periodic signal
2.Matlab code for sampling and recunstruciton
- 2012-07-29 15:44:01下载
- 积分：1
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fir_filter
用c#编写了一套FIR窗口滤波器，其中数据段的提取来自于matlab的混合编程(Written in c# a FIR filter window, including data extracted from the mixture of matlab programming)
- 2013-12-04 12:38:40下载
- 积分：1
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IntroductionForMatlab
说明： 本书全面的介绍了MATLAB的基础知识，对初学者很有用。(This book a comprehensive introduction to the basics of MATLAB for beginners useful.)
- 2010-03-28 17:32:21下载
- 积分：1
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rls
这个程序关于语音信号的消噪，实现了一个基于递归最小二乘法的自适应噪声抵消器(This program about the speech signal de-noising, implements a recursive least squares based adaptive noise canceller)
- 2013-07-27 11:16:49下载
- 积分：1
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System-identification-
系统辨识与自适应控制方面的matlab仿真程序，共6个章节(System identification and adaptive control matlab simulation program, a total of six chapters)
- 2012-10-19 22:05:30下载
- 积分：1
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guidesign
利用matlab设计gui界面实现对图像的平滑、锐化、反转等处理(Using matlab design GUI interface processing for image smoothing, sharpening, reverse)
- 2013-04-28 14:57:23下载
- 积分：1
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Digital-Signal-Processing-Using-Matlab-v4
Digital signal processing using matlab...e book useful for students............
- 2014-01-05 04:13:32下载
- 积分：1
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适用于捷联惯导系统(SINS)初始对准的新算法self-alignment
在运载体运动情况下,提出了一种适用于捷联惯导系统(SINS)初始对准的新算法,该算法以惯性空
间为过渡参考基准,即建立了初始时刻惯性坐标系(i0系)和初始时刻捷联惯组惯性坐标系(ib0系)两个惯性坐标
系。将捷联惯组坐标系(b系)与导航坐标系(n系)之间的初始对准姿态矩阵的实现分解为三步骤:(1)通过地理
位置和初始对准时间求解i0系至n系的变换矩阵 (2)通过惯导比力方程变形,引入测速仪速度辅助,求解从ib0
系至i0系的常值变换矩阵 (3)使用姿态更新算法实时计算b相对于ib0系的变换矩阵。最后,载车运动环境下的
初始对准试验结果表明航向角对准精度达到了0.1b(1R)。
(On the moving base, a new initial alignment algorithm for strapdown inertial navigation system
(SINS) is proposed. In this algorithm, two special inertial frames, the initia-l time inertial frame (i0frame) and
the initia-l time SINS body inertial frame (ib0frame), are defined and are selected as transition reference frames.
The calculation of initial alignment direction cosine matrix (DCM) between SINS body frame (bframe) and nav-
igation reference frame (nframe) is expanded into three parts: (1) the DCM betweeni0frame andnframe is
easily obtained via local geographical coordinates and initial alignment time (2) by expressing SINS specific
force equation inbframe and by the aid of external velocity log, the constant DCM fromib0frame toi0frame is
achieved (3) attitude updating using gyro samples gets the DCM betweenbframe andib0frame. In the end,
some vehicular tests are carried out on the moving base and the accuracy of azimuth reaches about 0.1b(1R).
)
- 2015-08-23 07:58:59下载
- 积分：1
