Description: 用于自适应控制的模糊神经网络代码，输入是误差和误差变化率。-for adaptive control of the FNN code, the importation of error and error rate of change. Platform: |
Size: 1024 |
Author:许佳 |
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Description: 自适应控制的一些MATLAB例子，也包含模糊控制的一些例子-adaptive control of MATLAB example, fuzzy control also includes some examples Platform: |
Size: 51200 |
Author:郑研 |
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Description: 自适应控制的例程
文件samp.m使用matlab6.5通过-adaptive control routines samp.m documents through the use of matlab6.5 Platform: |
Size: 1024 |
Author:zhangmcn |
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Description: 三容水箱的模糊控制设计，连接pc2006数据卡，运用模糊控制和自适应控制水位，利用vc＋＋编写界面。-three-tank design of fuzzy control, connectivity pc2006 data card, fuzzy control and adaptive control of the water level, using vc++ interface. Platform: |
Size: 3581952 |
Author:vicki |
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Description: 运用模型参考的方法实现自适应控制的!采用lypanuov稳定性理论来设计参数的调节-use of the model reference adaptive control method! Lypanuov stability theory used to design Parameter adjustment Platform: |
Size: 4096 |
Author:大荣 |
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Description: 步进电机自适应控制中的非线形问题,智能控制方法的应用-stepper motor adaptive control of non-linear problems, intelligent application of the control method Platform: |
Size: 278528 |
Author:雨刷 |
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Description: 基于RBF网络直接模型参考自适应控制，可以参考！希望能对大家有所帮助-direct model reference adaptive control, reference! The hope is to help everyone Platform: |
Size: 1024 |
Author:luchen |
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Description: 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 Platform: |
Size: 2045952 |
Author:zhouyang |
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Description: 对模型参考自适应进行仿真，并且给出控制算法的改进-The model reference adaptive simulation, and gives the control algorithm
Platform: |
Size: 2048 |
Author:李江业 |
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Description: 《系统辨识与自适应控制》程序，包含最小二乘辨识，模型参考自适应控制和自校正控制等-"System identification and adaptive control procedures, including the least squares identification, model reference adaptive control and self-tuning control Platform: |
Size: 2265088 |
Author:ZHC |
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