matlab中用FFT实现线性卷积循环卷积

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全部Solomon标准数据,txt格式,用于研究VRP问题.包含56个文件.

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本程序有算例分析，详细介绍了三种优化SVM方法：遗传算法、PSO、网格搜索法

传统的全景图像拼接算法，多采用 Harris 角点的特征提取或尺度不变特征转换 (SIFT)的特征匹配算子的方式，对存在重合部分的图像进行图像拼接处理。但对于车载全景图像拼接算法而言，车身四周采集到的 4 幅鱼眼畸变图像，使用特征提取算子的方法进行的拼接，运算的复杂度高，效率低，不能满足车载设备的实时性要求。针对这一问题，该文提出一种专门应用在车载系统的车载全景图像拼接算法，并对其进行 Matlab 仿真，最大限度提高算法的运算效率，以满足车载系统实时性的要求，真实的反应路况信息，辅助驾驶员安全驾驶。关键词：计算机视觉；图像拼接；车载全景；实时性；鱼眼图像

ViBe背景建模Matlab代码实现，只完成了比较基础的部分，但与官网的实现方式差不多，速度比较快。

10分绝对值。本人的详细制作报告，详细的介绍了语音信号的各种参数的特性和提取方法，并附上了源程序。以及各个调试阶段的仿真图分析。

频谱仪的介绍、操作及性能指标，硬件工程师必须学会的测量器件之一。Definitions and conditionsSpecifications describe the performance of parameters covered by the productwarranty and apply to the full temperature of 0 to 55C, unless otherwisenotedGet more Information95th percentile values indicate the breadth of the population (approx. 2 o) of perfor-This EXA signalanalyzer datamance tolerances expected to be met in 95 percent of the cases with a 95 percentsheet is a summary of theconfidence, for any ambient temperature in the range of 20 to 30C. In addition tothe statistical observations of a sample of instruments, these values include thespecifications and conditionseffects of the uncertainties of external calibration references these values are notfor N9010A EXA and N9010AEPwarranted. These values are updated occasionally if a significant change in theExpress EXA signal analyzers.statistically observed behavior of production instruments is observedwhich are available in the EXASignalAnalyzer SpecificationTypical describes additional product performance information that is not covered byGuide(N9010-90025)the product warranty It is performance beyond specifications that 80 percent of theunits exhibit with a 95 percent confidence level over the temperature range 20 toFor ordering informationkrefer30C. Typical performance does not include measurement uncertaintyto the EXA Signal AnalyzerConfiguration GuideNominal values indicate expected performance, or describe product performance59896531Nthat is useful in the application of the product, but are not covered by the productwarrantyThe analyzer will meet its specifications whenIt is within its calibration cycleUnder auto couple control, except when Auto Sweep Time rules= AccySignal frequencies 10 MHZ, with DC coupling appliedThe analyzer has been stored at an ambient temperature within the allowedoperating range for at least two hours before being turned on; if it had previouslybeen stored at a temperature range inside the allowed storage range, but outsidethe allowed operating rangeThe analyzer has been turned on at least 30 minutes with auto align set tonormal, or, if Auto align is set to off or partial, alignments must have been runrecently enough to prevent an Alert message; if the Alert condition is changedfrom Time and Temperature to one of the disabled duration choices, the analyzermay fail to meet specifications without informing the userFor the complete specifications guide, visitwww.agilent.com/find/exaspecifications1. For earlier instruments/Serial number prefix MY/SG/US5052), the full temperature rangesfrom5t50°CFrequency and Time specificationsFrequency rangeDC coupledAC coupledOption 50310 Hz to 3.6 Gh10 MHz to 3. 6 GHzOption 50710 Hz to 7 GH10 MHz to 7 GHzOption 51310 Hz to 13.6 GHz10 MHz to 13.6 ghzOption 52610 Hz to 26.5 GH10 MHz to 26.5 GhzOption 53210 Hz to 32 gHzNAOption 54410 Hz to 44 gHzNABandLO multiple(N)10 Hz to 3. 6 GHz3.5to7.0GH3.5to8.4GH28.4 to 13.6 GHz3135to17.1GH17 to 26.5 GHz5426.4 to 34.5 ghz344t044GHzFrequency referenceAccuracy+l time since last adjustment x aging rate)+ temperature stability t calibrationaccuracyAging rateOption pFrStandardy±1×106/year±15X107/2 yearsTemperature stabilityOption PFrStandard20to30°c±15×108±2×106Full temperature range±5x1±2×10Achievable initial calibration accuracyOption PFrStandard±4x108±1410Example trequency reterence accuracy=±(1×107+5×103+4×10-)(with Option PFR1 year after last adjustment±19x10Residual fmOption pFr

本文对捷联惯导系统(SINS)及其与全球定位系统(GPS)的组合导航系统进行了研究。导航传感器(加速度计、陀螺仪和GPS接收机)的各部分信息送入导航计算机，应用卡尔曼滤波方法进行数据处理后得到最优导航信息。本文首先对实现SINS初始对准这个关键技术进行了研究，实现了基参数辨识法的卡尔曼滤波初始精对准算法，大大提高了初始对准的精度。然后在此基础上进行了实现捷联惯导系统的软件编制，并对捷联惯导系统的误差进行了深入研究。最后在实现SINS的基础上，深入分析了GPS的误差来源，并建立了GPS误差模型，同时也研究了SINS与GPS的位置、速度组合导航，建立全球定位系统和捷联惯导系统的误差方程及位置速度测