The Application of Embedded Systems to Control Quad-Rotor Aircraft

The objective of this study was to design, engineer and develop a prototype of a quad-rotor aircraft. By applying embedded systems MCU ATMEGA2560 to control operation 5 flight experiments were conducted using the mission planner program to determine the position of a quad-roto aircraft, which studied 6-14 way point factors. The study area was Rajamangala University of Technology Rattanakosin. Wang Klai Kangwon Campus, Hua Hin District Prachuap Khiri Khan Province. The results of the study showed that the quad-rotor aircraft can fly according to the specified point position coordinates with the accuracy of 10-12 way point to 100% accuracy, 6 way point’s to 83.33%, 8 points to 87.50% and 14 points to 78.57. % with total average accuracy of 89.88%