modell

在Flash中实现使用滚动条控制文字滚动的动画+源文件，文字段落滚动，滚动条在文字左侧显示，拖动滚动条即可控制文字区域的文字向上、或向下滚动，用了一些Flash ActionScript脚本，仅供参考。

用友HRP固定资产岗位操作手册（带图）

这是CCS学习资料，有需要的尽情下载吧，里面介绍了CCS里的C语言编程-learning materials, it is necessary to download it enjoyable, they introduced the CCS The C Programming Language

旅行商算法，实现从加权有向图中寻找并输出最短的闭合路径(Traveling salesman algorithm, from a weighted directed graph to find and output the shortest path closure)

GSM半数率源代码(VSELP) GSM半数率源代码(VSELP) -GSM half rate of the source code (VSELP) GSM half rate of the source code (VSELP)

基于c8051平台，at25f512flash芯片测试程序-C8051-based platform, at25f512flash chip test program

说明：  matlab上基于ICA的故障监测程序，有注释(ICA-based fault monitoring)

实现新浪微博系统的基本功能，包括注册用户管理，发表心情，上传照片，发私信以及前台表单验证。 项目技术架构：项目采用自定义的仿Struts框架的web系统开发模式，应用MVC的三层体系结构，使系统可以便捷的进行业务扩展和适应变化的业务需求(Sina microblogging system s basic functions, including registered user management, published mood, upload photos, send private messages, and the front desk form validation. Project technical architecture: The project uses Struts framework imitation custom web system development model, the application of MVC three-tier architecture, the system can be convenient for business expansion and to adapt to changing business needs)

说明：  源代码；Python量化投资从入门到实战(source code; Practical Quant Investment in Python from Scratch)

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)