Nonlinear energy-based control method for aircraft dynamics

Nonlinear energy-based control method for aircraft dynamics

In this paper, we approach control of aircraft dynamics from an energy perspective. The method is based on the passivity-based control technique, and similar to Total Energy Control Systems (TECS). The aircraft dynamics are presented through the energy functions. By modifying these functions, st...

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Main Authors: Akmeliawati, Rini, Mareels, I.
Format: Conference or Workshop Item
Language:English
Published: 2002
Subjects:
TJ212 Control engineering
Online Access:http://irep.iium.edu.my/5400/
http://irep.iium.edu.my/5400/
http://irep.iium.edu.my/5400/
http://irep.iium.edu.my/5400/1/cdc2001.pdf
id iium-5400
recordtype eprints
spelling iium-54002012-01-24T23:52:45Z http://irep.iium.edu.my/5400/ Nonlinear energy-based control method for aircraft dynamics Akmeliawati, Rini Mareels, I. TJ212 Control engineering In this paper, we approach control of aircraft dynamics from an energy perspective. The method is based on the passivity-based control technique, and similar to Total Energy Control Systems (TECS). The aircraft dynamics are presented through the energy functions. By modifying these functions, stabilisation and tracking can be achieved. The method is illustrated on an automatic landing system problem for a twin-engine civil aircraft, developed by Group for Aeronautical Research and Technology in Europe (GARTEUR). To deal with the separation of the short-period and the phugoid dynamics, we use ideas from singular perturbation theory. Disturbance rejection and robustness analysis are performed via Monte Carlo simulations. The proposed control laws behave well even under extreme flight conditions 2002 Conference or Workshop Item PeerReviewed application/pdf en http://irep.iium.edu.my/5400/1/cdc2001.pdf Akmeliawati, Rini and Mareels, I. (2002) Nonlinear energy-based control method for aircraft dynamics. In: 40th IEEE Conference on Decision and Control, 2001, 04 Dec 2001 - 07 Dec 2001 , Orlando, FL , USA . http://dx.doi.org/10.1109/.2001.980179 doi:10.1109/.2001.980179
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
Akmeliawati, Rini
Mareels, I.
Nonlinear energy-based control method for aircraft dynamics
description In this paper, we approach control of aircraft dynamics from an energy perspective. The method is based on the passivity-based control technique, and similar to Total Energy Control Systems (TECS). The aircraft dynamics are presented through the energy functions. By modifying these functions, stabilisation and tracking can be achieved. The method is illustrated on an automatic landing system problem for a twin-engine civil aircraft, developed by Group for Aeronautical Research and Technology in Europe (GARTEUR). To deal with the separation of the short-period and the phugoid dynamics, we use ideas from singular perturbation theory. Disturbance rejection and robustness analysis are performed via Monte Carlo simulations. The proposed control laws behave well even under extreme flight conditions
format Conference or Workshop Item
author Akmeliawati, Rini
Mareels, I.
author_facet Akmeliawati, Rini
Mareels, I.
author_sort Akmeliawati, Rini
title Nonlinear energy-based control method for aircraft dynamics
title_short Nonlinear energy-based control method for aircraft dynamics
title_full Nonlinear energy-based control method for aircraft dynamics
title_fullStr Nonlinear energy-based control method for aircraft dynamics
title_full_unstemmed Nonlinear energy-based control method for aircraft dynamics
title_sort nonlinear energy-based control method for aircraft dynamics
publishDate 2002
url http://irep.iium.edu.my/5400/
http://irep.iium.edu.my/5400/
http://irep.iium.edu.my/5400/
http://irep.iium.edu.my/5400/1/cdc2001.pdf
first_indexed 2023-09-18T20:13:59Z
last_indexed 2023-09-18T20:13:59Z
_version_ 1777407664766058496

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