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Pchannel_resampling
nearest Neighbor Interpolator
- 2011-05-31 20:25:46下载
- 积分：1
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Prediction
混沌时间序列预测神经网络一步预测神经网络多步预测(chaotic time series predictionMain_RBF_MultiStepPred.m)
- 2013-11-26 16:30:22下载
- 积分：1
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BRI_patternhw5
brain computer interface
matlab code
- 2010-11-22 08:53:11下载
- 积分：1
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box_frac_dem
说明： 混沌理论盒维数的计算，MATLAB语言环境(Chaos theory calculation of box dimension, MATLAB language environment)
- 2010-05-03 10:12:09下载
- 积分：1
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LocalityPreservingProjections
matlab 的lpp的人脸识别，有训练库和测试库，里面还有文档说明
- 2010-05-24 18:13:58下载
- 积分：1
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Dataproc
利用田纳西伊斯曼过程数据 分析得到误差的特征统计量(
允许输入拉丁字符的拼音
中文(简体)
英语
日语
Tennessee Eastman process of data analysis to get the characteristics of the error statistics
允许输入拉丁字符的拼音
中文(简体)
英语
日语
Tennessee Eastman process of data analysis to get the characteristics of the error statistics)
- 2012-02-10 14:42:27下载
- 积分：1
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APF_ip_iq
这是一个APF仿真模型，谐波检测采用ipiq方法，电流跟踪控制采用滞环控制，直流侧电压为PI控制(This is an APF simulation model, harmonic detection using ipiq method, the current tracking control using hysteresis control, DC side voltage for the PI control)
- 2017-04-02 11:57:50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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ch44
- implementation d ue commande par mode glissant -
- 2015-02-23 22:04:34下载
- 积分：1
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221237351720061192258333067065
说明： 光流算法代码，实现对单运动目标，多运动目标的检测(optical flow code)
- 2009-08-31 17:54:57下载
- 积分：1
