-
FDTD_PML_1D_v5
一维正弦调制脉冲传播演示，PML吸收 a a a (a one demension sin wave demonstration, PML absorbed boundary a a a a a a a a a a)
- 2009-09-04 17:13:21下载
- 积分：1
-
logistic
说明： 求Lyapunov指数，LOGISITIC映射(Seek Lyapunov index, LOGISITIC map)
- 2010-04-08 17:22:48下载
- 积分：1
-
radar_system_simulation
雷达系统分析主要包括脉冲压缩、相干积累、非相干积累、CFAR、脉冲测角(Radar systems analysis including pulse compression, coherent accumulation, non-coherent accumulation, CFAR, pulse goniometer)
- 2013-12-15 12:43:19下载
- 积分：1
-
BP1
BP神经网络实现图像压缩，用的matlab语言，图像处理中很常用的(BP neural network image compression, using matlab language, very commonly used in image processing)
- 2015-04-13 08:49:02下载
- 积分：1
-
Vector-control
本模型是基于异步电机矢量控制的仿真实验，并附有word详细解释模型的建立过程，以及仿真结果（波形）。(This model is based on the simulation experiment of asynchronous motor vector control, accompanied by the word detailed explanation model establishment process, and simulation results (waveform).)
- 2020-10-21 14:37:24下载
- 积分：1
-
ode
matlab codes for solving ODEs, including euler method, RK methods etc, and some examples.
- 2007-09-22 23:31:15下载
- 积分：1
-
1001conv_enc_Viterbi_dec
一种高速卷积编码技术及其Viterbi译码技术研究(A high-speed convolutional coding and Viterbi decoding technology technology research)
- 2008-05-04 10:26:57下载
- 积分：1
-
Reconfigurable-flight-control
精密控制结构需要满足先进飞机的使命和对其引航的要求。这就要求飞行器的性能必须满足在低空飞行，低速飞行和大迎角攻击性飞行，全天候，昼夜工作的条件，并且新的控制技术应该成熟。这项工作提出了飞行控制时，状态变量和控制输入是由预先确定的限制范围内的系统控制系统的设计理念。在设计过程使用动态规划的概念。其基本思想涉及非二次泛函最小化。由于一系列限制因素，建议使用光滑函数。同时提出了该综合方法的优点。我们利用对F-18战斗机的纵向控制配置来说明该设计方法。(Indirect adaptive control for reconfigurable flight control is advocated. Specifically,
online static system identification using a moving window/batch estimation is implemented.
The ensuing linear regression is augmented with an intercept. The intercept parameter is
included to address the effects of trim change associated with the occurrence of a control surface
failure. Parameter estimate information is used to adjust the inner loop’s control gains, and
a command derived from the intercept estimate is fed forward to automatically retrim the aircraft.
The tracking performance of this automatic retrimming method, which relies on system
identification, surpasses the conventional approach of exclusively relying on integral action
for retrimming. These adaptive and reconfigurable flight control concepts are illustrated in
the context of a fighter aircraft’s pitch plane dynamics. The novel adaptive and reconfigurable
flight control system successfully handles a 50 per cent horiz)
- 2011-05-02 12:39:11下载
- 积分：1
-
Array_antenna_study
阵列分析与综合入门代码，含比较好的绘图模块(Array analysis with the entry code, with better graphics module)
- 2013-03-04 17:50:37下载
- 积分：1
-
epllcode
This code implements the algorithm described in the paper:
Blind deblurring using internal patch recurrence
by Tomer Michaeli and Michal Irani
- 2014-11-24 15:28:02下载
- 积分：1
