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Experimental feedback linearisation of a non-smooth nonlinear system by the method of receptances

Domenico Lisitano, Shakir Jiffri Orcid Logo, Elvio Bonisoli, John E Mottershead

Mathematics and Mechanics of Solids, Volume: 24, Issue: 4

Swansea University Author: Shakir Jiffri Orcid Logo

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DOI (Published version): 10.1177/1081286517744601

Abstract

Input–output partial feedback linearisation is experimentally implemented on a non-smooth nonlinear system without the necessity of a conventional system matrix model for the first time. The experimental rig consists of three lumped masses connected and supported by springs with low damping. The inp...

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Published in: Mathematics and Mechanics of Solids
ISSN: 1081-2865 1741-3028
Published: 2018
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URI: https://cronfa.swan.ac.uk/Record/cronfa36830
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first_indexed 2017-11-20T14:26:05Z
last_indexed 2020-07-14T13:02:58Z
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spelling 2020-07-14T11:37:39.6720258 v2 36830 2017-11-20 Experimental feedback linearisation of a non-smooth nonlinear system by the method of receptances 1d7a7d2a8f10ec98afed15a4b4b791c4 0000-0002-5570-5783 Shakir Jiffri Shakir Jiffri true false 2017-11-20 AERO Input–output partial feedback linearisation is experimentally implemented on a non-smooth nonlinear system without the necessity of a conventional system matrix model for the first time. The experimental rig consists of three lumped masses connected and supported by springs with low damping. The input and output are at the first degree of freedom with a non-smooth clearance-type nonlinearity at the third degree of freedom. Feedback linearisation has the effect of separating the system into two parts: one linear and controllable and the other nonlinear and uncontrollable. When control is applied to the former, the latter must be shown to be stable if the complete system is to be stable with the desired dynamic behaviour. Journal Article Mathematics and Mechanics of Solids 24 4 1081-2865 1741-3028 Active vibration control, receptance method, non-smooth nonlinearity, feedback linearisation 31 12 2018 2018-12-31 10.1177/1081286517744601 COLLEGE NANME Aerospace Engineering COLLEGE CODE AERO Swansea University 2020-07-14T11:37:39.6720258 2017-11-20T11:03:28.3411040 Faculty of Science and Engineering School of Aerospace, Civil, Electrical, General and Mechanical Engineering - Aerospace Engineering Domenico Lisitano 1 Shakir Jiffri 0000-0002-5570-5783 2 Elvio Bonisoli 3 John E Mottershead 4 0036830-09022018133214.pdf lisitano2018.pdf 2018-02-09T13:32:14.9970000 Output 2114341 application/pdf Version of Record true 2018-02-09T00:00:00.0000000 This article is distributed under the terms of the Creative Commons Attribution 4.0 License true eng http://www.creativecommons.org/licenses/by/4.0/
title Experimental feedback linearisation of a non-smooth nonlinear system by the method of receptances
spellingShingle Experimental feedback linearisation of a non-smooth nonlinear system by the method of receptances
Shakir Jiffri
title_short Experimental feedback linearisation of a non-smooth nonlinear system by the method of receptances
title_full Experimental feedback linearisation of a non-smooth nonlinear system by the method of receptances
title_fullStr Experimental feedback linearisation of a non-smooth nonlinear system by the method of receptances
title_full_unstemmed Experimental feedback linearisation of a non-smooth nonlinear system by the method of receptances
title_sort Experimental feedback linearisation of a non-smooth nonlinear system by the method of receptances
author_id_str_mv 1d7a7d2a8f10ec98afed15a4b4b791c4
author_id_fullname_str_mv 1d7a7d2a8f10ec98afed15a4b4b791c4_***_Shakir Jiffri
author Shakir Jiffri
author2 Domenico Lisitano
Shakir Jiffri
Elvio Bonisoli
John E Mottershead
format Journal article
container_title Mathematics and Mechanics of Solids
container_volume 24
container_issue 4
publishDate 2018
institution Swansea University
issn 1081-2865
1741-3028
doi_str_mv 10.1177/1081286517744601
college_str Faculty of Science and Engineering
hierarchytype
hierarchy_top_id facultyofscienceandengineering
hierarchy_top_title Faculty of Science and Engineering
hierarchy_parent_id facultyofscienceandengineering
hierarchy_parent_title Faculty of Science and Engineering
department_str School of Aerospace, Civil, Electrical, General and Mechanical Engineering - Aerospace Engineering{{{_:::_}}}Faculty of Science and Engineering{{{_:::_}}}School of Aerospace, Civil, Electrical, General and Mechanical Engineering - Aerospace Engineering
document_store_str 1
active_str 0
description Input–output partial feedback linearisation is experimentally implemented on a non-smooth nonlinear system without the necessity of a conventional system matrix model for the first time. The experimental rig consists of three lumped masses connected and supported by springs with low damping. The input and output are at the first degree of freedom with a non-smooth clearance-type nonlinearity at the third degree of freedom. Feedback linearisation has the effect of separating the system into two parts: one linear and controllable and the other nonlinear and uncontrollable. When control is applied to the former, the latter must be shown to be stable if the complete system is to be stable with the desired dynamic behaviour.
published_date 2018-12-31T03:46:11Z
_version_ 1763752198040190976
score 11.013148

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