Disclosed are a glider, a simple wind tunnel, a webcam, and an experimental system for educating aircraft stability using a computer and a method therefor. Aircraft stability analysis system according to an embodiment of the present invention is a wind tunnel device for generating wind; an aircraft connected to the wind tunnel device by a connecting means and whose motion is changed by the wind generated by the wind tunnel device; a first photographing means for photographing an image for analyzing a pitch motion of the aircraft; a second photographing means for photographing an image for analyzing a roll motion and a yaw motion of the aircraft; And by analyzing the image taken by the first shooting means and the second shooting means to analyze the change in pitch motion, roll motion and yaw motion with respect to the vehicle, the analyzed pitch motion, roll motion with respect to the vehicle And control means for analyzing the stability of the vehicle based on the change in the yaw motion, wherein the vehicle is the head of the vehicle through the connecting means to limit the translational motion of the vehicle and leave only the rotational motion component The part and the wind tunnel device are connected.
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