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于 2010-11-09 发布 文件大小:23442KB
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  matlab基础教程,比较适合新手学习使用(matlab basic tutorial, suitable for beginners learning to use)

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    说明:  通信系统方面的matlab书籍,对通信系统相关方面都有涉及,是用matlab仿真通信系统的教材.(Communication systems matlab books related to aspects of the communication system involved is the simulation of communication systems using matlab materials)
    2010-04-22 19:39:27下载
    积分:1
  • immumatlab
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    2010-05-05 09:19:36下载
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    2011-07-04 21:39:59下载
    积分:1
  • STBC_MIMO_code
    STBC MIMO 通信的代码,模拟了不同SNR下的BER。代码中,有注释说明(STBC MIMO communication code to simulate the BER in the SNR. Code, there are explanatory notes)
    2012-05-24 17:31:33下载
    积分:1
  • BLDC_Control
    In This Matlab Simulation, We simulate Control System Of BLDC Motor Speed Control With Addaptive Fuzzy Sliding Mode Control And Simulatione Show That The result is better than other Control Method Such as Conventional PID.
    2013-02-18 23:04:46下载
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    Aplicaç ã o MySQL estúdio musical
    2014-11-20 01:25:05下载
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  • SVM1alloptimization
    SVM 1 to all optimization process matlab code
    2015-01-20 05:58:39下载
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  • 魔术公式轮胎模型
    魔术轮胎模型在simulink中的应用。。。。。。。。。。。。(Simulink model of magic tire in MATLAB)
    2017-06-28 10:00:33下载
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  • bin
    曲线拟合系统,输入阶数进行拟合计算和插值计算(Curve fitting system to fit the input order of calculation and interpolation)
    2011-05-07 15:57:38下载
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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
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