DESAIN DAN SIMULASI KONTROL KECEPATAN MOTOR QUADCOPTER

This paper discusses a design of the motor speed control to regulate the stability of motion an altitude Vertical Take-off quadcopter. The control design is determined by load and lift force speed. Vertical Take-off was derived by using the Euler Newton method. Proportional Integral Derivative PID controller is proposed to control the stability of quadcopter motion and MATLAB Simulink is used to validate the control design. The simulation result shows that the PID controller obtains the best speed response compared with the PI controller.