This is a program helps in preliminary aircraft design and optimization. It is an object-oriented MATLAB program can a) Visualize an aircraft design b) Get important aircraft performance parameters (left coefficent, stability derivatives, etc. ) c) Get important aircraft performance graphs (Cl/Cd graph, Drag/speed graph, etc. )
- Please read "Brief Intro to MATLAB Code" to get more details about the code.
- "mainExample.m" construct a example aircraft. Run it. The "testUAV" object is the aircraft builded based on given parameters.
The example is a design for mission like "Fulton Skyhook" The following example image is an overview of the final design of the aircraft.