Performance comparisons between PID and adaptive PID controllers for travel angle control of a bench-top helicopter
This paper provides a comparative study on the performances of standard PID and adaptive PID controllers tested on travel angle of a 3-Degree-of-Freedom (3-DOF) Quanser bench-top helicopter. Quanser, a well-known manufacturer of educational bench-top helicopter has developed Proportional Integration...
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iium-410632015-07-12T04:00:57Z http://irep.iium.edu.my/41063/ Performance comparisons between PID and adaptive PID controllers for travel angle control of a bench-top helicopter Mansor, Hasmah Mohd Noor, Samsul Bahari Gunawan, Teddy Surya Khan, Sheroz Othman, N. I. Tazali, N. Islam, R. B. T Technology (General) This paper provides a comparative study on the performances of standard PID and adaptive PID controllers tested on travel angle of a 3-Degree-of-Freedom (3-DOF) Quanser bench-top helicopter. Quanser, a well-known manufacturer of educational bench-top helicopter has developed Proportional Integration Derivative (PID) controller with Linear Quadratic Regulator (LQR)for all travel, pitch and yaw angle of the bench-top helicopter. The performance of the PID controller is relatively good; however, its performance could also be improved if the controller is combined with adaptive element. The objective of this research is to design adaptive PID controller and then compare the performances of the adaptive PID with the standard PID. The controller design and test is focused on travel angle control only. Adaptive method used in this project is self-tuning controller, which controller’s parameters are updated online. Two adaptive algorithms those are pole-placement and deadbeat have been chosen as the method to achieve optimal controller’s parameters. Performance comparisons have shown that the adaptive (deadbeat) PID controller has produced more desirable performance compared to standard PID and adaptive (poleplacement). The adaptive (deadbeat) PID controller attained very fast settling time (5 seconds) and very small percentage of overshoot (5% to 7.5%) for 10° to 30° step change of travel angle. Research Science Press 2015-01-26 Article PeerReviewed application/pdf en http://irep.iium.edu.my/41063/1/Waset_Jeddah_Published.pdf Mansor, Hasmah and Mohd Noor, Samsul Bahari and Gunawan, Teddy Surya and Khan, Sheroz and Othman, N. I. and Tazali, N. and Islam, R. B. (2015) Performance comparisons between PID and adaptive PID controllers for travel angle control of a bench-top helicopter. International Journal of Electronics, Electrical and Communication Engineering, 9 (1). pp. 35-40. ISSN 0975-4814 http://www.waset.org/Publications/?path=Publications&p=97 |
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T Technology (General) Mansor, Hasmah Mohd Noor, Samsul Bahari Gunawan, Teddy Surya Khan, Sheroz Othman, N. I. Tazali, N. Islam, R. B. Performance comparisons between PID and adaptive PID controllers for travel angle control of a bench-top helicopter |
description |
This paper provides a comparative study on the performances of standard PID and adaptive PID controllers tested on travel angle of a 3-Degree-of-Freedom (3-DOF) Quanser bench-top helicopter. Quanser, a well-known manufacturer of educational bench-top helicopter has developed Proportional Integration Derivative (PID) controller with Linear Quadratic Regulator (LQR)for all travel, pitch and yaw angle of the bench-top helicopter. The performance of the PID controller is relatively good; however, its performance could also be improved if the controller is combined
with adaptive element. The objective of this research is to design adaptive PID controller and then compare the performances of the adaptive PID with the standard PID. The controller design and test is focused on travel angle control only. Adaptive method used in this project is self-tuning controller, which controller’s parameters are
updated online. Two adaptive algorithms those are pole-placement and deadbeat have been chosen as the method to achieve optimal controller’s parameters. Performance comparisons have shown that the adaptive (deadbeat) PID controller has produced more desirable performance compared to standard PID and adaptive (poleplacement).
The adaptive (deadbeat) PID controller attained very fast
settling time (5 seconds) and very small percentage of overshoot (5% to 7.5%) for 10° to 30° step change of travel angle. |
format |
Article |
author |
Mansor, Hasmah Mohd Noor, Samsul Bahari Gunawan, Teddy Surya Khan, Sheroz Othman, N. I. Tazali, N. Islam, R. B. |
author_facet |
Mansor, Hasmah Mohd Noor, Samsul Bahari Gunawan, Teddy Surya Khan, Sheroz Othman, N. I. Tazali, N. Islam, R. B. |
author_sort |
Mansor, Hasmah |
title |
Performance comparisons between PID and adaptive PID controllers for travel angle control of a bench-top helicopter |
title_short |
Performance comparisons between PID and adaptive PID controllers for travel angle control of a bench-top helicopter |
title_full |
Performance comparisons between PID and adaptive PID controllers for travel angle control of a bench-top helicopter |
title_fullStr |
Performance comparisons between PID and adaptive PID controllers for travel angle control of a bench-top helicopter |
title_full_unstemmed |
Performance comparisons between PID and adaptive PID controllers for travel angle control of a bench-top helicopter |
title_sort |
performance comparisons between pid and adaptive pid controllers for travel angle control of a bench-top helicopter |
publisher |
Research Science Press |
publishDate |
2015 |
url |
http://irep.iium.edu.my/41063/ http://irep.iium.edu.my/41063/ http://irep.iium.edu.my/41063/1/Waset_Jeddah_Published.pdf |
first_indexed |
2023-09-18T20:58:49Z |
last_indexed |
2023-09-18T20:58:49Z |
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