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Rayleigh
本例程为matlab实现的单径或多径瑞利衰落信道仿真的几种例程(Matlab routines for the realization of the single-track trails or Rayleigh fading channel simulation of several routines)
- 2020-09-21 09:17:54下载
- 积分：1
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cp0801_PAMreceiver
超宽带脉冲幅度调制接收端频谱，与其他的几个共用(Ultra-wideband pulse amplitude modulation spectrum receiver, and some other common)
- 2009-03-26 20:22:10下载
- 积分：1
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SPAN-system-based-on-gesture-detection-method
SPAN系统的姿态检测方法SPAN system based on gesture detection method(SPAN system based on gesture detection method)
- 2011-01-10 19:27:26下载
- 积分：1
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QR_factorization
These are the QR/RQ factorization techniques required for the Zero forcing detection technique for MIMO.
- 2010-03-12 02:46:32下载
- 积分：1
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Random-signal-processing
随机信号处理，包括各种概率计算，各种功率谱计算(Random signal processing, including all probability, a variety of power spectrum)
- 2010-07-01 22:07:46下载
- 积分：1
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MATLAB
卷积运算：取x(t)和h(t)的长度为nx,nh。平移量n=nh+nx-1，利用for和if语句实现倒序求和运算。外循环用一个for语句实现平移，通过在求和时取数组元素的顺序实现倒序求和(Convolution operation: take x (t) and h (t) of length nx, nh. Translational volume n = nh+ Nx-1, use for and if statements to achieve reverse summation operator. Outside the circle with a for statement to achieve translation, when taken in sum array elements to achieve reverse the order of summation)
- 2007-11-15 07:21:36下载
- 积分：1
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chapter13
matlab30个案例算法之一，对学习有很大帮助(the one of matlab30 case algorithm learning)
- 2012-08-29 10:59:57下载
- 积分：1
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zidongkongzhi
自动控制原理PPT大学教程，是华北电力大学的(Automatic control theory PPT university course, is North China Electric Power University)
- 2013-12-25 20:32:38下载
- 积分：1
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fsk1
基于matlab的2fsk的调制与解调源程序，以及眼图，误码率的计算，相干解调，非相干解调的比较(Matlab-based 2fsk the source of the modulation and demodulation, as well as the eye diagram, bit error rate calculation, coherent demodulation, comparison of non-coherent demodulation)
- 2009-05-02 16:45:31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
