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jiefangchengzu
快速解方程组,用MATLAB解方程组,快捷!(Rapid solution equations, solution of equations with MATLAB, fast!)
- 2008-07-01 08:50:32下载
- 积分:1
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deploy_001
无线网络节点的部署,还是又障碍物版的,可以方便您编程,节省时间(Deployment of wireless network nodes, or another version of the obstacles can be programmed for your convenience and save time)
- 2011-08-19 22:30:39下载
- 积分:1
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v5-code
localization for WSN
- 2011-08-23 18:27:08下载
- 积分:1
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capitalreturn
资本市场 市场线 预测市场风险 matlab预测(Capital markets, market line forecast market risk)
- 2013-02-03 20:08:25下载
- 积分:1
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adequacy-analysis
Adequacy analysis with DG(Wind Turbine) using monte carlo simulation.Average unsupplied load(AUL)is calculated for annual load demand
- 2020-12-07 20:59:20下载
- 积分:1
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alp_bet_convv
This model is very much useful in converting the normal three phase voltages to the corresponding alpha beta components
- 2013-12-11 13:46:43下载
- 积分:1
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ImageFrequencyFiltering
Frequncy Filtering in digital image processing
- 2015-04-11 00:02:44下载
- 积分:1
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moead_(WS,TE,PBI)
说明: moead源代码,包括三种分解方式,WS,TE,PBI(Moead source code, including three decomposition methods)
- 2020-10-31 19:49:55下载
- 积分:1
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polyphase_deng
基于多相滤波的信道化接收机DDC MATLAB仿真程序。(Based polyphase filter of the receiver channel DDC MATLAB simulation program.)
- 2009-05-20 19:45:11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