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Butterworth_Filter
butterworth滤波器，可实现高通低通滤波(butterworth filter, low pass filter high-pass)
- 2010-11-04 21:54:58下载
- 积分：1
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38-jawaban-seo
38 pertanyaan tentang Search Engine Optimizer dan jawaban mengenai pertanyaan itu.
- 2010-11-22 16:18:19下载
- 积分：1
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simmm1
SIMMM1 simulate a M/M/1 queueing system. Poisson arrivals of intensity lambda. Poisson service times S of intensity mu.
- 2009-05-25 16:33:40下载
- 积分：1
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digitalsignalprocessing
胡广书《数字信号处理-理论，算法和实现》第二版光盘内容，覆盖所有章节课后习题内容(Hu Guang book " Digital Signal Processing- theory, algorithms and implementation," Second Edition CD-ROM content, covering all sections of the content of after-school exercise)
- 2010-05-20 10:20:43下载
- 积分：1
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DSPshiyan
精心编写的信号处理的实验指导书，程序在matlab上运行。(Signal processing and well-written experimental instructions, the program running in matlab.)
- 2012-05-17 17:24:18下载
- 积分：1
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MATLAB仿真
最基础的风力机模型和光伏电池模型，适合入门者(The most basic wind turbine model and photovoltaic cell model, suitable for beginners)
- 2021-04-26 18:18:45下载
- 积分：1
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Orbital_compute
进行航天器轨道运算经常用到的函数，包括坐标转换，经纬度转换，二体运动，轨道要素计算等等(For spacecraft orbit operations frequently used functions, including coordinate conversion, latitude and longitude conversion, two-body movement, and so calculated orbital elements)
- 2020-07-01 02:20:02下载
- 积分：1
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RealTimeClock
Guide for DS1307 Real Time Clock
- 2010-12-22 00:35:25下载
- 积分：1
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17days_all
本资料为杨鹏老师所编，内涵了gre词汇的背诵方法，以及以前版本所没有的易混单词，实为难得的好材料(the book mainly describes an effective way to recite GRE words.)
- 2010-03-09 17:18:24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
