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A simulated intelligent controller for aircraft pitch control

International Conference on Man Machine Systems (ICoMMS 2012) organized by School of Mechatronic Engineering, co-organized by The Institute of Engineer, Malaysia (IEM) and Society of Engineering Education Malaysia, 27th - 28th February 2012 at Bayview Beach Resort, Penang, Malaysia.

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Bibliographic Details
Main Authors: Fahisal, Abdullah, Siti Marhainis, Othman, Nasrul Helmei, Halim
Other Authors: fahisal@unimap.edu.my
Format: Working Paper
Language:English
Published: Universiti Malaysia Perlis (UniMAP) 2012
Subjects:
Intelligent controller
PID controller
Fuzzy logic controller
MATLAB simulink
MATLAB GUI
Online Access:http://dspace.unimap.edu.my/xmlui/handle/123456789/20504
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spelling my.unimap-205042012-07-19T14:50:37Z A simulated intelligent controller for aircraft pitch control Fahisal, Abdullah Siti Marhainis, Othman Nasrul Helmei, Halim fahisal@unimap.edu.my Intelligent controller PID controller Fuzzy logic controller MATLAB simulink MATLAB GUI International Conference on Man Machine Systems (ICoMMS 2012) organized by School of Mechatronic Engineering, co-organized by The Institute of Engineer, Malaysia (IEM) and Society of Engineering Education Malaysia, 27th - 28th February 2012 at Bayview Beach Resort, Penang, Malaysia. This paper is present about a simulated intelligent controller for aircraft pitch control. This project uses two types of controllers such as PID controller and fuzzy logic controller. Both types of controllers will be compared to the best results can be obtained. The purpose is to use the controller for controlling the aircraft pitch angle. Results shown in MATLAB Simulink. This project is a closed loop system. Where there are step, controller, plant, output and feedback. PID controller have three term controller such as Proportional gain (Kp), Integral gain (Ki) and Derivative gain (Kd). Fuzzy logic controller (FLC) is a second controller in this project. This controller developed for control the pitch of an aircraft system. Simulation results with respect to the response of the pitch angle and pitch rate are presented based on common’s criteria of step response. Finally, the performances of pitch control systems are examined and analyzed in terms of percent of overshoot, rise time, settling time and steady state error in order to identify how good the response of the controller. GUI will be developed by using MATLAB to view the response of the simulated of pitch control system. 2012-07-19T14:50:35Z 2012-07-19T14:50:35Z 2012-02-27 Working Paper http://hdl.handle.net/123456789/20504 en Proceedings of the International Conference on Man-Machine Systems (ICoMMS 2012) Universiti Malaysia Perlis (UniMAP) School of Mechatronic Engineering
institution Universiti Malaysia Perlis
building UniMAP Library
collection Institutional Repository
continent Asia
country Malaysia
content_provider Universiti Malaysia Perlis
content_source UniMAP Library Digital Repository
url_provider http://dspace.unimap.edu.my/
language English
topic Intelligent controller
PID controller
Fuzzy logic controller
MATLAB simulink
MATLAB GUI
spellingShingle Intelligent controller
PID controller
Fuzzy logic controller
MATLAB simulink
MATLAB GUI
Fahisal, Abdullah
Siti Marhainis, Othman
Nasrul Helmei, Halim
A simulated intelligent controller for aircraft pitch control
description International Conference on Man Machine Systems (ICoMMS 2012) organized by School of Mechatronic Engineering, co-organized by The Institute of Engineer, Malaysia (IEM) and Society of Engineering Education Malaysia, 27th - 28th February 2012 at Bayview Beach Resort, Penang, Malaysia.
author2 fahisal@unimap.edu.my
author_facet fahisal@unimap.edu.my
Fahisal, Abdullah
Siti Marhainis, Othman
Nasrul Helmei, Halim
format Working Paper
author Fahisal, Abdullah
Siti Marhainis, Othman
Nasrul Helmei, Halim
author_sort Fahisal, Abdullah
title A simulated intelligent controller for aircraft pitch control
title_short A simulated intelligent controller for aircraft pitch control
title_full A simulated intelligent controller for aircraft pitch control
title_fullStr A simulated intelligent controller for aircraft pitch control
title_full_unstemmed A simulated intelligent controller for aircraft pitch control
title_sort simulated intelligent controller for aircraft pitch control
publisher Universiti Malaysia Perlis (UniMAP)
publishDate 2012
url http://dspace.unimap.edu.my/xmlui/handle/123456789/20504
_version_ 1643793092949573632
score 13.214268

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