通过将用户友好交互的飞机建模与快速空气动力学分析相结合，本程序直观地描述了各种设计参数如何影响飞机的飞行方式。
By interfacing user-friendly aircraftmodeling with rapid aerodynamic analysis, this program visually depicts howvarious design parameters affect the way an airplane flies.
MathWorks网站上验证该代码的视频网址如下：
A video demonstrating some of the code’scapabilities can be found on the MathWorks website at https://www.mathworks.com/videos/matlab-and-simulink-robotics-arena-building-interactive-design-tools-1509569729395.html.
除了在调整飞机模型时更新的内置线性稳定近似值之外，程序还支持与下列软件进行接口，以便进行更高级的分析：
In addition to built-in, linearizedstability approximations that are updated every time the aircraft model isadjusted, the program interfaces with the following software for more advancedanalysis:
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Digital DATCOM –U.S.Air Force -
Tornado Vortex Lattice Method –Tomas Melin (KTH Royal Institute of Technology) -
AVL (Athena Vortex LatticeMethod) – Mark Drela and Harold Youngren (MIT)
本代码还可以通过以下开源软件获得附加的其它功能：
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DATCOM Plot InterpolationFunctions – Prof. Glenn Greiner and Lenny Gartenberg (ERAU, Daytona Beach, FL) -
AVL Input/Output Functions –Joseph Moster (Mathworks File Exchange) -
Datcomimport – MathWorksAerospace Toolbox – loads DATCOM "for006.dat" file -
NACA456 – Ralph Carmichael(PDAS) – calculates NACA 6-series airfoil ordinates
工具箱插件下载地址：
http://page5.dfpan.com/fs/clcbj2c21e29f16c9e1/
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