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events_matlab
传感器网络探测声信号通过特征提取进行目标设别分类(Sensor network to detect acoustic signals through the feature extraction for target-based classification of other)
- 2007-08-07 10:25:26下载
- 积分：1
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Meshing_Fractures
岩体稳定性计算，裂隙岩体节理网络网格划分，用于有限元计算。应用于边坡，大坝等岩体结构工程！(Rock stability calculation, fractured rock joint network mesh for finite element calculations. Applied to the slope, dams and other rock structure works!)
- 2014-09-17 12:49:46下载
- 积分：1
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hedge
国债期货的套期保值matlab代码示例,利用wind数据导入matlab，含套保率图形(Hedging matlab code examples bond futures)
- 2015-04-12 21:42:02下载
- 积分：1
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新建文本文档
copula函数 模型建立 相关性分析 模型拟合检验(Establishment of correlation analysis by copula function model)
- 2018-03-23 16:26:56下载
- 积分：1
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rcj10j0008_m3tsra74v410
瑞萨数据手册指令集瑞萨数据手册指令集瑞萨数据手册指令集(zhilingji)
- 2010-01-22 15:01:43下载
- 积分：1
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MATLAB-command
matlab教程，matlab参考书，学习matlab必备啊！(matlab for study.)
- 2013-09-03 21:19:02下载
- 积分：1
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start
评分打星星的一个例子 可以用来参考 很实用(An example of playing star ratings can be used to refer to)
- 2011-11-12 12:09:29下载
- 积分：1
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000000GAU
genetic algorithm solve optimization
- 2015-01-17 21:07:49下载
- 积分：1
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simplex_2steps
最优化算法中，单纯形表法+两步法的matlab实现，通过两个实例调用两个函数实现(Optimization algorithm, matlab tableau method+ two-step method of implementation, call the two functions by means of two examples of the realization)
- 2015-07-06 16:39:30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
