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oneclass
用于将不规则的数据分类 整理 实用性很强 适用于各种经济模型(Irregular data is used to sort out are very practical for a variety of economic models)
- 2008-07-01 11:43:25下载
- 积分:1
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Untitledcapon2m
关于二维Capon算法的研究,对于学习空间谱估计的同学有参考价值(On the two-dimensional Capon algorithm for learning spatial spectral estimation of the students have reference value)
- 2016-11-10 11:55:31下载
- 积分:1
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sift
SIFT (scale invariant feature transform)
- 2010-10-28 19:44:14下载
- 积分:1
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amd
matlab程序语言,三自由度模型对象,主动控制,lqr算法,求解位移与速度(the matlab programming languages, three degrees of freedom model objects, active control, lqr algorithm solving the displacement and velocity)
- 2013-01-04 11:15:33下载
- 积分:1
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LCMV 圆阵 circle3
LCMV 圆阵 实现均匀圆阵的 俯仰角 水平角 视图(LCMV circular array for horizontal angle of pitch angle of uniform circular array.)
- 2018-04-06 21:11:06下载
- 积分:1
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PI_adjust
单相并网逆变器,使用无源阻尼,实现并网电流波形和电网电压波形同频同相(Single-phase grid-connected inverters, using passive damping, realize grid-connected current waveform and grid voltage waveform in the same frequency and phase)
- 2019-04-26 16:39:24下载
- 积分:1
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matlab
matlab book for bigenners very useful
- 2010-07-20 20:02:52下载
- 积分:1
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First_Best_Next_Worst_fit
计算机内存分配,首次适应策略、最佳适应策略、循环适应策略、最坏适应策略。matlab代码,略简单(Storage Allocation First_fit/Best_fit/Next_fit/Worst_fit)
- 2013-04-17 16:04:36下载
- 积分:1
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NAGS2-matlab-code
NAGS2的代码,解决多目标优化问题,多目标问题可自己写,也可以我提供的,我只是提供了几个简单的多目标问题(NAGS2 code, solve the problem of multi-objective optimization, multi-objective problem can write your own, or you can provide me, I just offer a few simple multi-objective problem)
- 2021-01-15 16:38:50下载
- 积分:1
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月球软着陆程序
说明: 月球软着陆仿真:在停泊轨道上,探测器在脉冲制动的作用下,经霍曼变轨,下降到距月面大约 15 公里的近月点,该近月点就是主制动段的初始制动点。主制动段以下是障碍检测与规避和最终着陆段。在主制动段,由于探测器的初始速度很大(1.692km/s),所以主制动段制导律设计的主要目的就是高效抵消此速度,将探测器导引到期望的末端状态(Lunar soft landing simulation: in the parking orbit, the probe under the action of pulse braking, through the hohmann change of orbit, to descend to about 15 kilometers from the surface of the moon, the near-moon point is the main braking section of the initial braking point. Following is the main braking section for obstacle detection and avoidance and the final landing section. In the main braking section, since the initial velocity of the detector is very large (1.692km/s), the main purpose of the guidance law design of the main braking section is to effectively offset this velocity and guide the detector to the desired terminal state)
- 2021-01-28 22:18:35下载
- 积分:1