Roll and yaw stabilisation using nonlinear energy method

Automatic flight control systems have become increasingly vital ever since the emergence of airplanes. Automatic systems are not subject to fatigue and emotions as compared to the human pilot. As such, the possibility of human errors in flight control is minimized. Current automatic Flight Contro...

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Main Authors: Lim, Jen Nee Jones, Akmeliawati, Rini, Chee, Pin Tan
Format: Conference or Workshop Item
Language:English
Published: 2007
Subjects:
Online Access:http://irep.iium.edu.my/5286/1/icarcv2006.pdf
http://irep.iium.edu.my/5286/
http://dx.doi.org/10.1109/ICARCV.2006.345124
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spelling my.iium.irep.52862012-05-23T01:59:53Z http://irep.iium.edu.my/5286/ Roll and yaw stabilisation using nonlinear energy method Lim, Jen Nee Jones Akmeliawati, Rini Chee, Pin Tan TJ212 Control engineering TK Electrical engineering. Electronics Nuclear engineering Automatic flight control systems have become increasingly vital ever since the emergence of airplanes. Automatic systems are not subject to fatigue and emotions as compared to the human pilot. As such, the possibility of human errors in flight control is minimized. Current automatic Flight Control Systems are designed based on classical control theories using linear controllers that are complex and inefficient. Since an aircraft is naturally nonlinear in its behavior, it is intuitive to design a nonlinear controller that could cover a wide variety of possible ‘extreme’ flight conditions. A novel controller utilizing the Nonlinear Energy Method was developed by Akmeliawati for the longitudinal dynamics of an aircraft, and has been proven to provide effective control and better performance when compared to an equivalent linear controller. The novel controller was designed using the Passivity-Based Control (PBC) technique. In this paper, a similar nonlinear controller was designed to direct the roll and yaw motion, which is part of the lateral dynamics of the aircraft. Simulations show that this PBC is able to stabilize both roll and yaw motion of the aircraft. 2007 Conference or Workshop Item REM application/pdf en http://irep.iium.edu.my/5286/1/icarcv2006.pdf Lim, Jen Nee Jones and Akmeliawati, Rini and Chee, Pin Tan (2007) Roll and yaw stabilisation using nonlinear energy method. In: 9th International Conference on Control, Automation, Robotics and Vision, 2006. ICARCV '06. , 5-8 Dec. 2006 , Singapore. http://dx.doi.org/10.1109/ICARCV.2006.345124 doi:10.1109/ICARCV.2006.345124
institution Universiti Islam Antarabangsa Malaysia
building IIUM Library
collection Institutional Repository
continent Asia
country Malaysia
content_provider International Islamic University Malaysia
content_source IIUM Repository (IREP)
url_provider http://irep.iium.edu.my/
language English
topic TJ212 Control engineering
TK Electrical engineering. Electronics Nuclear engineering
spellingShingle TJ212 Control engineering
TK Electrical engineering. Electronics Nuclear engineering
Lim, Jen Nee Jones
Akmeliawati, Rini
Chee, Pin Tan
Roll and yaw stabilisation using nonlinear energy method
description Automatic flight control systems have become increasingly vital ever since the emergence of airplanes. Automatic systems are not subject to fatigue and emotions as compared to the human pilot. As such, the possibility of human errors in flight control is minimized. Current automatic Flight Control Systems are designed based on classical control theories using linear controllers that are complex and inefficient. Since an aircraft is naturally nonlinear in its behavior, it is intuitive to design a nonlinear controller that could cover a wide variety of possible ‘extreme’ flight conditions. A novel controller utilizing the Nonlinear Energy Method was developed by Akmeliawati for the longitudinal dynamics of an aircraft, and has been proven to provide effective control and better performance when compared to an equivalent linear controller. The novel controller was designed using the Passivity-Based Control (PBC) technique. In this paper, a similar nonlinear controller was designed to direct the roll and yaw motion, which is part of the lateral dynamics of the aircraft. Simulations show that this PBC is able to stabilize both roll and yaw motion of the aircraft.
format Conference or Workshop Item
author Lim, Jen Nee Jones
Akmeliawati, Rini
Chee, Pin Tan
author_facet Lim, Jen Nee Jones
Akmeliawati, Rini
Chee, Pin Tan
author_sort Lim, Jen Nee Jones
title Roll and yaw stabilisation using nonlinear energy method
title_short Roll and yaw stabilisation using nonlinear energy method
title_full Roll and yaw stabilisation using nonlinear energy method
title_fullStr Roll and yaw stabilisation using nonlinear energy method
title_full_unstemmed Roll and yaw stabilisation using nonlinear energy method
title_sort roll and yaw stabilisation using nonlinear energy method
publishDate 2007
url http://irep.iium.edu.my/5286/1/icarcv2006.pdf
http://irep.iium.edu.my/5286/
http://dx.doi.org/10.1109/ICARCV.2006.345124
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