均值滤波去噪

GIMP中文手册 (Chinese GIMP manual)

这是一个书籍管理应用程序。系统要完成对书籍的管理，应包括类目管理：书籍的增加和删除；借阅管理：借出和还入；信息的查询等功能。-This is a book management application. To complete the system of management books, including Category Management : books on the increase and deleted; Readers management : the lending and also means; Information inquiries, and other functions.

说明：  python读取csv 文件，提供了神经网络的程序，以及自编码器(Python reading CSV file)

该应用程序向导创建的测试应用程序为您服务。该文件包含测试应用程序组件每个文件摘要的内容。Test.vcproj这是使用应用程序向导生成的VC++项目的主项目文件。它包含有关该文件的Visual C++版本的信息的产生的信息，并关于向导选择应用程序平台，配置和项目信息的功能。TEST.CPP这是主要的应用源文件。////////////////////////////////////////////////// ///////////////////////////其他标准文件：StdAfx.h中，StdAfx.cpp这些文件被用于生成名称test.pch预编译头（PCH）文件，名为StdAfx.obj式预编译的文件。////////////////////////////////////////////////// ///////////////////////////其他意见：应用程序向导使用“TODO：”注释指示应添加或源代码的定制部件。

说明：  用于在abaqus中建立平面内随机分布的椭圆的py代码(a python script for abaqus, which can be used to build a large numeber of random ellipsoids.)

C# LumiSoft.Net的源码库 和网上找的一个Sip电话实例 有需要的可以看看 LumiSoft.Net的协议还是很丰富的，希望可以帮到大家(C# LumiSoft. Net source library and a Sip phone instance found on the Internet need to see LumiSoft. Net protocol is still very rich, I hope to help you.)

说明：  i wish most help you to find this file thanks

Ucos Operating system for Lcd 9"

说明：  This is a Solid Works Model to a Brick Maker

NSEG是美国兰利研究中心推出的飞行器起飞、爬升、巡航、加速、下降、减速和着陆等各个过程分析软件。(NSEG was developed to perform rapid aircraft mission analyses. It is based upon the use of approximate equations of motion whose form varies with the type of flight segment. Flight segments considered are takeoff, accelerations, climbs, cruises, descents, decelerations, and landings. Layered atmosphere options are available. The program can also be used for flight envelope mapping. NSEG provides the capability to analyze aircraft missions from low to hypersonic speeds. Realistic and detailed vehicle characteristics are input to NSEG to permit accurate mission analysis. NSEG allows engine scaling so as to fit the design under analysis. NSEG contains several approximate flight path optimization capabilities based on Rutowski energy-like criteria for considering minimum time or fuel flight segments and maximum range segments during climb or descent. Takeoff and landing analysis is based on the Air Force Flight Dynamics Laboratory DATCOM method of high lift aerodynamic modelling)