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kalmaneasystuding
kalman递归理论的详细讲解,通谷易懂,想弄明白kalman理论的同志一看便知!(a easy understanding for Kalman theory.it is very useful for new leaner! )
- 2010-12-30 13:35:39下载
- 积分：1
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s_pal_rls_amplitude
RLS自适应数字预失真算法Matlab仿真，仿真通过，比较少见的资料，仅供学习交流(Matlab simulation of RLS adaptive digital distortion algorithm for PA)
- 2021-03-18 14:49:20下载
- 积分：1
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MATLAB
truetime工具箱2.0 bate6里面的例子(The examples of Truetime 2.0 bate 6)
- 2012-05-03 13:31:17下载
- 积分：1
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renal-artery-input-function
Renal artery input function(AIF) fitting tool.
It s used for mice Contrast-enhanced MR image.
- 2011-07-20 17:23:50下载
- 积分：1
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Simulink
Aspen Dynamics 与Simulink 联合仿真的案例学习(Design and Cosimulate Control of Distillation Tower with Aspen Plus Dynamics- MATLAB & Simulink Example)
- 2021-03-18 12:29:21下载
- 积分：1
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matlab-
解决多目标线性问题 解决多目标带约束条件的例子(To solve the multi-objective linear problem)
- 2013-03-20 19:29:35下载
- 积分：1
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mdl
fuzzy logic is a good controller
- 2014-02-19 02:26:58下载
- 积分：1
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MATLABMINGLING
MATLAB命令大全，非常简单实用的教程。适合初学者使用，()
- 2008-04-10 11:03:27下载
- 积分：1
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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
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Matlab-PSO
To find and estimate of the best solution and parameter in our problem we can use the evolutionary programming. PSO (particle swarm optimization) is an applicable method to catch this target.
In these files I show the Simple PSO that it can be base of solve complicated problem, the code could run by MATLAB.
- 2013-07-15 01:15:42下载
- 积分：1
