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用于图像识别的2DPCA算法程序(matlab)
利用2DPCA进行图像的降维处理,有PCA所不具备的保持图像几何特征的性质。同时,运算速度也比PCA快。经过2DPCA线性降维器降维后,方便进行分类识别。代码是matlab编程
- 2020-12-04下载
- 积分:1
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PX4-Pixhawk程序研究笔记
系统的了解Pixhawk的原生固件PX4
- 2021-05-06下载
- 积分:1
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NGUI v3.12.1 2018 最新版NGUI
2018最新版NGUI 版本 v3.12.1 2018-6-28 更新 NGUI Next-Gen UI v3.12.1.unitypackage
- 2020-12-12下载
- 积分:1
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LabView虚拟仪器数据采集与串口通信测控应用实战.(人民邮电.李江全等).(配书源码)
《LabView虚拟仪器数据采集与串口通信测控应用实战》(人民邮电出版社.李江全.刘恩博.胡蓉)一书的配套源代码。
- 2020-12-08下载
- 积分:1
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曲柄连杆的运动分析(MATLAB源代码)
只需改函数的原始参数就可以分析各种曲柄连杆机构的运动,包括角位移,角速度,角加速度,和运动仿真
- 2020-12-09下载
- 积分:1
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Julia程序设计
lia (编程语言) Julia 是一个面向科学计算的高性能动态高级程序设计语言。其语法与其他科学计算语言相似。在许多情况下拥有能与编译型语言相媲美的性能。Julia 是个灵活的动态语言,适合科学和数值计算,性能可与传统静态类型语言媲美。
- 2021-05-06下载
- 积分:1
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phaseSpaceReconstruction.m
【实例简介】相空间重构函数,该函数的作用是自动得到时间序列重构时需要的参数:延迟时间和嵌入维数。
- 2021-11-07 00:38:27下载
- 积分:1
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计算机二级Msoffice往年真题
计算机二级Msoffice往年真题
- 2021-05-07下载
- 积分:1
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主要针对CPU模拟卡进行了代码优化.注意只有PN532能用
CPU模拟卡工具,只要针对的模拟卡进行了优化.为用卡安全提供参考.
- 2020-11-28下载
- 积分:1
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Datcom说明书
计算飞机气动特性的软件的说明书,主要应用于概念设计和初步设计阶段TABLE 2AERODYNAMIC OUTPUT AS A FUNCTION OF /CONFIGURATION AND SPEED REGIME● OUTPUT A∨A| LABLED OUTPUT ONLY FOR CON FIGURATIONS WITH STRAIGHT TAPERED SURFACESA OUTPUT ONLY WITH EXPERIMENTAL DATA INPUCONFIGURATION SPEEDSTATIC AERODYN AMIC CHARACTERISTIC OUTPUTDY NAMIC STABILITY CUTPUREGIMECLSUBSONICBODYTRANSONICSUPERSONICHY PERSONICWINGTRANS0NC口▲|口「口百口SUPERSONIC●{a!口口日口HYPERSONIC口!口D口口HORIZONTALTRANS0NCa|▲▲口口|口白SUPERSONIC·a|口口口·『●|●IY PERSONICVERTICAL TAILSUBSONICOR VENTRALTRANSONIC口FINA sUPERSONIC.「百|口HY PERSONICSUBSONICWING-BODYRANSONC口口口o口SUPERSONIC●d|口HY PERSON百口HORIZONTALTRANS0NIc口口口TAIL- BOOYSUPERSONIC口口0口HY PERSONICSUBSONICVERTICAL TAILTRANSONIC口VENTRAL FIN-2 SUPERSONIC.BODY●●|●|●HYPERSONIC口w|NG-B0D¥△ SUBSONIC■口|口|口|口|a口|aaa0|口aaaaTRANSONICO|口TAILSUPERS0NC口百|百口「口。|口HYPERS0NC口口|口口口口口口SUBSON1C●VERTICAL TAILTRANS0NC▲口VENTRAL FINA SUPERSONIC●●|●●HYPERSONICING BOOYSUBSONICHORIZONTAL口日|a口口a「aa}aTRANSONIC|▲|▲▲▲口A SUPERSONIC O。|。口}口|口口|口VERTICAL TAILVENTRAL FINHYPERS0NC口口c1 THE EFFECTS OF JET POW2PELLER POWER, AND GROUND PROXIMITY MAY BE OBTAINED FOR THESE CONFIGURATIONS IF THE REQUIREDNAMELISTS ARE INPUT, THE EFFECTS OF POWER AND GROUND EFFECTS ARE INCLUDED ONLY IN THE SU!C LONGI TUDIN AL STABILITY RESULTS2 DY NAMIC STABILITY RESULTS ARE THE SAME AS WING-BODY3 TKIN VERTICAL TAIL RESULTS MAY BE OBTAINED FOR THESE CONFIGURATIONS IF THE REQUIRED NAMELIST IS INPUTTHESE EFFECTS ARE INCLUDED ONLY IN THE SUBSONIC LATERAL STABILITY DATAREFER TO DATCOM HANDBOOK FOR METHOD LIMITATIONS IF OUTPUT IS NOT OBTAINED5 AVAILABLE ONLY IN COMBINAT:ON WITH A WING OR TAILCC
- 2020-12-12下载
- 积分:1