Control of twin-lift helicopter system

The control of a twin-lift helicopter system with and without spreader bar is addressed in this thesis. Fist, the two and three dimensional models of the system are presented. Then three different control schemes are considered; these schemes consist of a PID control law, a robust control law and a...

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Bibliographic Details
Main Author:	Lye, Cheng Lin.
Other Authors:	Mohamed Zribi
Format:	Theses and Dissertations
Published:	2010
Subjects:	DRNTU::Engineering::Electrical and electronic engineering::Control and instrumentation
Online Access:	http://hdl.handle.net/10356/38992
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Institution:	Nanyang Technological University

id	sg-ntu-dr.10356-38992
record_format	dspace
spelling	sg-ntu-dr.10356-389922023-07-04T15:27:26Z Control of twin-lift helicopter system Lye, Cheng Lin. Mohamed Zribi School of Electrical and Electronic Engineering DRNTU::Engineering::Electrical and electronic engineering::Control and instrumentation The control of a twin-lift helicopter system with and without spreader bar is addressed in this thesis. Fist, the two and three dimensional models of the system are presented. Then three different control schemes are considered; these schemes consist of a PID control law, a robust control law and a variable structure control law. The simulations of the system with the different control laws are carried out using the UH-60 helicopter parameters. The simulations for the spreader bar and the non-spreader bar configurations are discussed. It was found that regardless of the configuration of the twin-lift helicopter system, the variable structure control law achieves better performances than the PID and robust control laws. Master of Science (Computer Control and Automation) 2010-05-21T03:39:06Z 2010-05-21T03:39:06Z 1997 1997 Thesis http://hdl.handle.net/10356/38992 NANYANG TECHNOLOGICAL UNIVERSITY 192 p. application/pdf
institution	Nanyang Technological University
building	NTU Library
continent	Asia
country	Singapore Singapore
content_provider	NTU Library
collection	DR-NTU
topic	DRNTU::Engineering::Electrical and electronic engineering::Control and instrumentation
spellingShingle	DRNTU::Engineering::Electrical and electronic engineering::Control and instrumentation Lye, Cheng Lin. Control of twin-lift helicopter system
description	The control of a twin-lift helicopter system with and without spreader bar is addressed in this thesis. Fist, the two and three dimensional models of the system are presented. Then three different control schemes are considered; these schemes consist of a PID control law, a robust control law and a variable structure control law. The simulations of the system with the different control laws are carried out using the UH-60 helicopter parameters. The simulations for the spreader bar and the non-spreader bar configurations are discussed. It was found that regardless of the configuration of the twin-lift helicopter system, the variable structure control law achieves better performances than the PID and robust control laws.
author2	Mohamed Zribi
author_facet	Mohamed Zribi Lye, Cheng Lin.
format	Theses and Dissertations
author	Lye, Cheng Lin.
author_sort	Lye, Cheng Lin.
title	Control of twin-lift helicopter system
title_short	Control of twin-lift helicopter system
title_full	Control of twin-lift helicopter system
title_fullStr	Control of twin-lift helicopter system
title_full_unstemmed	Control of twin-lift helicopter system
title_sort	control of twin-lift helicopter system
publishDate	2010
url	http://hdl.handle.net/10356/38992
_version_	1772828850617581568

Control of twin-lift helicopter system

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