PERANCANGAN INTERFACE QUADCOPTER BERBASIS ARDUINO DENGAN KONTROL PID

Abstract

UAV (Unmanned Aerial Vehicle) or commonly called unmanned aircraft is currently experiencing very rapid development in the world. The use of UAVs is categorized quite broadly starting from the needs of military surveillance, mapping, research, aerial photography or just a hobby. Quadcopter is one type of UAV aircraft that uses 4 rotors as a quadrotor. The balance control system uses PID, the Proportional Integral Derivative (PID) control system is a conventional controller used to determine the precision of a system with the characteristics of feedback on the system. The PID control system consists of three, namely Proportional, Integral and Derivative. Flight test results by giving one by one values to the roll axis, pitch, and yaw. PID roll and Pitch values are Kp 1.4, Ki 0.05, Kd 15 and the value of yaw Kp 4, Ki 0.02, Kd 0 which can help control flying stably.