Development of nonlinear energy-based method (NEM) controller for 3 DOF helicopter

Development of nonlinear energy-based method (NEM) controller for 3 DOF helicopter

In this paper, this design was a Nonlinear Energy-based Control Method (NEM) controller for a Three degree-of-freedom (3 DOF) Helicopter developed by Quanser. It is a control design technique that exploits the energy state of a system to achieve stabilization and/or tracking. There are four stages...

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Main Authors: , Pharmayeni, Akmeliawati, Rini, Legowo, Ari
Format: Conference or Workshop Item
Language:English
Published: 2011
Subjects:
TJ212 Control engineering
Online Access:http://irep.iium.edu.my/5393/
http://irep.iium.edu.my/5393/
http://irep.iium.edu.my/5393/
http://irep.iium.edu.my/5393/1/ICOM11_pharmayeni.pdf
id iium-5393
recordtype eprints
spelling iium-53932012-02-28T01:49:16Z http://irep.iium.edu.my/5393/ Development of nonlinear energy-based method (NEM) controller for 3 DOF helicopter , Pharmayeni Akmeliawati, Rini Legowo, Ari TJ212 Control engineering In this paper, this design was a Nonlinear Energy-based Control Method (NEM) controller for a Three degree-of-freedom (3 DOF) Helicopter developed by Quanser. It is a control design technique that exploits the energy state of a system to achieve stabilization and/or tracking. There are four stages to design NEM controller, which are: energy-based modeling of helicopter dynamics using Euler-Lagrange formalism; design of the NEM controller based on passivity principle and Lyapunov stability idea; tuning the controller gain(s) to satisfy the design criteria and robustness analysis. 2011 Conference or Workshop Item PeerReviewed application/pdf en http://irep.iium.edu.my/5393/1/ICOM11_pharmayeni.pdf , Pharmayeni and Akmeliawati, Rini and Legowo, Ari (2011) Development of nonlinear energy-based method (NEM) controller for 3 DOF helicopter. In: 2011 4th International Conference on Mechatronics: Integrated Engineering for Industrial and Societal Development (ICOM 2011), 17-19 May, 2011, Kuala Lumpur, Malaysia. http://dx.doi.org/10.1109/ICOM.2011.6016111 doi:10.1109/ICOM.2011.6016111
repository_type Digital Repository
institution_category Local University
institution International Islamic University Malaysia
building IIUM Repository
collection Online Access
language English
topic TJ212 Control engineering
spellingShingle TJ212 Control engineering
, Pharmayeni
Akmeliawati, Rini
Legowo, Ari
Development of nonlinear energy-based method (NEM) controller for 3 DOF helicopter
description In this paper, this design was a Nonlinear Energy-based Control Method (NEM) controller for a Three degree-of-freedom (3 DOF) Helicopter developed by Quanser. It is a control design technique that exploits the energy state of a system to achieve stabilization and/or tracking. There are four stages to design NEM controller, which are: energy-based modeling of helicopter dynamics using Euler-Lagrange formalism; design of the NEM controller based on passivity principle and Lyapunov stability idea; tuning the controller gain(s) to satisfy the design criteria and robustness analysis.
format Conference or Workshop Item
author , Pharmayeni
Akmeliawati, Rini
Legowo, Ari
author_facet , Pharmayeni
Akmeliawati, Rini
Legowo, Ari
author_sort , Pharmayeni
title Development of nonlinear energy-based method (NEM) controller for 3 DOF helicopter
title_short Development of nonlinear energy-based method (NEM) controller for 3 DOF helicopter
title_full Development of nonlinear energy-based method (NEM) controller for 3 DOF helicopter
title_fullStr Development of nonlinear energy-based method (NEM) controller for 3 DOF helicopter
title_full_unstemmed Development of nonlinear energy-based method (NEM) controller for 3 DOF helicopter
title_sort development of nonlinear energy-based method (nem) controller for 3 dof helicopter
publishDate 2011
url http://irep.iium.edu.my/5393/
http://irep.iium.edu.my/5393/
http://irep.iium.edu.my/5393/
http://irep.iium.edu.my/5393/1/ICOM11_pharmayeni.pdf
first_indexed 2023-09-18T20:13:58Z
last_indexed 2023-09-18T20:13:58Z
_version_ 1777407663896788992

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