Optimasi Pengendali PID pada Pesawat Autopilot Berbasiskan Algoritma Genetika

Nowadays, technology counts automation as one of the considerable features on it. The ability of machine to work independently become very important, like in aircraft industry. Aircrafts which able to decide their own path are called autopilot. In this research, the control system of pesawat was des...

Full description

Bibliographic Details
Main Author: Muhammad Ilhamdi Rusydi
Format: Article
Language:English
Published: Universitas Andalas 2016-07-01
Series:Jurnal Nasional Teknik Elektro
Subjects:
PID
Online Access:http://jnte.ft.unand.ac.id/index.php/jnte/article/view/267
Description
Summary:Nowadays, technology counts automation as one of the considerable features on it. The ability of machine to work independently become very important, like in aircraft industry. Aircrafts which able to decide their own path are called autopilot. In this research, the control system of pesawat was designed to keep it fly on the reference of high based on the pilot demands. Using the transfer function of aircraft, PID controller was designed based on genetic algorithm (PID-GA). The performance of PID-GA was compared to the PID which was tuned by Ziegler-Nichlos. The result showed that the chosen PID-GA which the threshold, generation and population are 10, 30, 50 performed better performance than PID-ZN. The parameter of proportional, integral and derivate controller are 9,66, 9,15 and 9.06. The specification of the system performance based on PID-GA were 0.55 second of rise time, 5.3 second of rise time. This result were better than the PID-ZN results. The system performance based on PID-ZN 0.732 second of rise time and 19.1 second of settling time.
ISSN:2302-2949
2407-7267