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sui_3_channel
simulation of sui channel model
- 2009-02-19 18:28:56下载
- 积分：1
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relation_dtft_dft_fft
说明连续时间傅里叶变换与DTFT、DFT之间的关系，及由FFT求连续时间傅里叶变换的方法。文档说明加MATLAB代码(This project is about the relationship of CTFT, DTFT and DFT, how to calculating CTFT by using FFT. This project contains document and matlab code.)
- 2012-09-21 19:52:31下载
- 积分：1
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ssc32-matlab
control SSC32 servo controller
- 2008-01-18 22:46:30下载
- 积分：1
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lslsvm--toolbox
matlab 最小二乘支持向量机 工具箱 有多个函数 可以用(matlab toolbox least squares support vector machine can)
- 2010-06-19 10:14:55下载
- 积分：1
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Split_Bregman_for_Snake
基于偏微分框架的全局快速活动轮廓分割模型(Framework based on partial differential global fast active contour segmentation model)
- 2010-10-07 04:35:17下载
- 积分：1
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poly_2string
polynomial coeff to string
- 2011-05-02 01:24:40下载
- 积分：1
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zero-finder.m
TESTZERO is a collection of nonlinear functions that may be used to test zero finders, that is, programs that seek a root of a scalar equation F(X)=0.
- 2011-05-04 08:46:44下载
- 积分：1
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Matlab信道模型
watterson信道matlab仿真,瑞利衰落。。。。(This example shows how to simulate High-Frequency (HF) ionospheric channels, based on the models described in Recommendation ITU-R F.1487. In particular, it shows how to simulate the general Watterson channel model, and other simplified channel models used in the quantitative testing of HF modems. It makes use of the Rayleigh multipath fading channel object and the Gaussian and bi-Gaussian Doppler structures from Communications System Toolbox.)
- 2021-04-23 22:28:47下载
- 积分：1
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QPSKsimulatorANDber
QPSK调制下在AWGN和Rayleigh衰落信道下的仿真以及误码率计算，包含完整的报告说明(QPSK modulation in AWGN and Rayleigh fading channel simulation, as well as bit error rate calculation, the report contains a complete description)
- 2020-07-02 23:20:01下载
- 积分：1
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LanderMission
这个课题设计从地球的近地轨道起飞到达谷神星预定轨道并且着陆在其表面上的一种数值方法。基于有限时间的航行纠正点火而非瞬时推力数值计算和Matlab仿真。最后可以看到空间飞行器从地球的影响球飞到谷神星的影响球的飞行轨迹。(This project explores the mathematical methods and results of designing a mission to land a spacecraft on the asteroid Ceres by beginning in an earth-centered LEO orbit and ending in an orbit prepared to land on the surface of the asteroid. Rather than assume instantaneous velocity changes, course-correcting burns of finite time are considered and analyzed using numerical methods and Matlab computation. The behavior of the spacecraft is observed inside the Earth s sphere of influence, in interplanetary space, and inside Ceres sphere of influence. )
- 2010-01-12 13:42:02下载
- 积分：1
