Simulasi Sistem Kontrol Autopilot pada Gerak Longitudinal Pesawat menggunakan Metode Pembentukan Lup PID

Abstract

Abstract PID controllers is the commonly used in industry, in instruments and laboratory equipment including aerospace subject. This controllers commonly used because it is easy to combine with another controllers. In this papers the controllers constants for Proportional controller K p , Integral controller Ki and Diferential controller Kd for obtain required systems for longitudinal motion of aircraft are determine by using loop shaping method where is the controller constans determine by analyze frequency respons of bode plot from plant. The advantage of loop shaping method is there is no need tuning for determine PID controllers constans.