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volvec
Run this m-file to see several examples of volume visualization in MATLAB.
- 2007-10-14 11:19:18下载
- 积分：1
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smoothing-filtering
采用3×3模板进行平滑滤波，去除噪声干扰(33 template smoothing filter to remove noise interference.)
- 2013-05-16 19:26:45下载
- 积分：1
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power_wind_dfig
9MW风电场simulink仿真模型，可直接运行(9MW wind farm simulink simulation model can be run directly)
- 2015-04-16 20:51:53下载
- 积分：1
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微分方程GUI
基于MATLAB的微分方程的界面设计，应付一下作业(Interface Design of Differential Equation Based on MATLAB)
- 2018-12-22 21:43:48下载
- 积分：1
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rotaplane_dynamic_model
说明： 六旋翼飞机模型，包含六旋翼飞行器的电机模型和动力学运动学模型，输入为六个电机的油门(Six-rotor aircraft model, including six rotor vehicle motor model and kinetic kinematics model, input six motor throttle)
- 2019-04-16 10:23:07下载
- 积分：1
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BPSK-QPSK
this code explains the bpsk and qpsk program.
in simulink design...
- 2012-05-03 18:28:52下载
- 积分：1
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MATLAB_programming_interpolation_and_curve_fitting
MATLAB程序设计插值及曲线拟合算法MATLAB programming interpolation and curve fitting algorithm(MATLAB programming interpolation and curve fitting algorithm MATLAB programming interpolation and curve fitting algorithm)
- 2010-08-02 10:28:53下载
- 积分：1
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duocifangzhenxiamubiaoguijdeMSE
多次仿真时目标轨迹的MSE,可以得到多次仿真时所有采样点的误差平均值的多个数据(MSE of target trajectory when simulated many times)
- 2013-11-30 11:32:54下载
- 积分：1
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Digital-beam-forming
画出下述情况下均匀线阵方向图
1）计算来波方向为0度方向图
2）画出来波方向为45度时的方向图
3）画出来波方向为0度，幅度取分贝数：20log***（单位为dB）时的方向图
4）画出来波方向为0度，随着阵元数的增加，当N=16，N=32时的方向图，并对方向图的变化情况进行说明(Draw the following conditions uniform linear array
1) calculation of wave direction is 0 degrees direction diagram
2) draw out the wave direction is 45 degrees direction map
3) draw out the wave direction is 0 degrees, and amplitude decibels: 20log*** (unit dB) when the direction of FIG.
4) draw out the wave direction is 0 degrees, with the increase of the number of array elements, when N=16, N=32 pattern, and the change of direction is described
)
- 2013-05-02 23:44:17下载
- 积分：1
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main
利用参数辨识法提取相关对准参数，从而估计出陀螺漂移和数学平台偏角并进行补偿。仿真结果表明，开路罗经法对准具有较高的对准精度、较好的快速性，能够满足捷联惯导系统在静基座下实现自对准的要求。(Expressions of mathematical platform misalignment angles of the open-loop algorithm are derived and parameter identification method is
used to pick-up the corresponding coefficients from angle measurements in order to identify and compensate gyro drifts and platform misalignment．The simulation results show that the open circuit gyrocompass alignment of SINS can all meet the requirement of SINS initial alignment with high accuracy and quick reaction on static base. thus can meet the high-precision alignment requirement of carrier based inertial navigation system on swinging base．
)
- 2014-02-09 15:52:36下载
- 积分：1
