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BPNN132U
超前校正环节,低界控制系统的超前控制算法,简单实用,MATLAB实现.(caoqianjiaozheng,control system.low order system,use in matlab,simple code,anyone can easy use it.)
- 2009-03-08 21:18:55下载
- 积分:1
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Attitude3D
identifacation systems
- 2013-07-16 19:58:12下载
- 积分:1
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pca-matlab
PCA又为主成分分析,是一种特征提取方法, 它通过线性变换寻找一组最优的单位正交向量基,用他们的线性组合来重构原样本(PCA and the main component analysis, a feature extraction method, which by finding a set of optimal linear transformation unit orthogonal base vectors, with their linear combination to reconstruct the original sample)
- 2011-06-30 16:55:43下载
- 积分:1
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Rotman_lens
计算Rotman_lens结构中馈电点的位置的matlab程式(calculate the position of feed point in rotman_lens)
- 2011-09-22 21:53:05下载
- 积分:1
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msquery_7
MS Query based application
- 2011-02-10 15:23:23下载
- 积分:1
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linkpidsimu
一个运用matlab程序源码,进行模糊PID设计 完整源码。(A program source code using matlab, the fuzzy PID design a complete source code.)
- 2011-04-19 11:44:56下载
- 积分:1
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matlab_code3
matlab下可以直接使用的小程序 包括各种常用算法 对应书籍为《matlab宝典》(matlab can be directly used for small programs, including such popular books as the corresponding algorithm " matlab Collection" )
- 2013-09-27 15:30:31下载
- 积分:1
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MATLAB
本书对matlab的基础及应用进行了详细介绍,适合matlab初学者学习。(The book and applications on the basis of matlab described in detail, suitable for beginners to learn matlab.)
- 2010-12-06 00:01:11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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fig2_SOM
四个光孤子的独立波解同时存在于一个方程中。这里是在MATLAB中的编程。(The independence of the four soliton wave solutions exist in a equation. Here is the programming in MATLAB.)
- 2010-06-18 20:12:53下载
- 积分:1