抄録
Recently, drones have been used in many areas. The object of this research is to make an automatic flight drone, find how the autopilot system controls the drone by investigating its aerodynamic characteristics. The method comprises designing and assembling a drone using Pixhawk, a flight controller; measuring its aerodynamics characteristics in a wind tunnel using a balance system; and analyzing the obtained data. The results clearly showed that the automatic flight system worked under various conditions. Further research is required to find the best PID tuning to adapt the drone to rapidly changing environments.
