Disturbance-observer-based fuzzy terminal sliding mode control for MIMO uncertain nonlinear systems

•Modelling and simulation of a novel five-rotor unmanned aerial vehicle with an extra rotor.•Proposing a disturbance-observer-based fuzzy terminal sliding mode controller.•Considering MIMO uncertain nonlinear systems with unmeasured external disturbance.•Unknown non-symmetric input saturation and co...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Veröffentlicht in:Applied Mathematical Modelling 2019-06, Vol.70, p.109-127
Hauptverfasser: Vahidi-Moghaddam, Amin, Rajaei, Arman, Ayati, Moosa
Format: Artikel
Sprache:eng
Schlagworte:
Online-Zugang:Volltext
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
container_end_page 127
container_issue
container_start_page 109
container_title Applied Mathematical Modelling
container_volume 70
creator Vahidi-Moghaddam, Amin
Rajaei, Arman
Ayati, Moosa
description •Modelling and simulation of a novel five-rotor unmanned aerial vehicle with an extra rotor.•Proposing a disturbance-observer-based fuzzy terminal sliding mode controller.•Considering MIMO uncertain nonlinear systems with unmeasured external disturbance.•Unknown non-symmetric input saturation and control singularity are investigated.•Closed-loop stability and convergence of the state estimations in finite time are proved. This study is concerned with the design of a disturbance-observer-based fuzzy terminal sliding mode controller (FTSMC) for multi-input multi-output (MIMO) uncertain nonlinear systems by considering unknown non-symmetric input saturation and control singularity. The disturbance observer is proposed for the unmeasured external disturbance and guarantees the convergence of the disturbance estimation error to zero in a finite time. The terminal sliding mode controller (TSMC) is designed for MIMO uncertain nonlinear systems by utilizing the output of the proposed disturbance observer. This control scheme combines the disturbance-observer-based TSMC with a fuzzy logic system in the presence of unknown non-symmetric input saturation and control singularity in order to reduce chattering phenomena. Finite time asymptotic stability, convergence of the disturbance observer, and convergence of the closed-loop system are proved via Lyapunov stability theorem. In addition, a five-rotor unmanned aerial vehicle (UAV) is employed in the numerical simulations to demonstrate the effectiveness and performance of the proposed control scheme. Disturbance observer estimates the payload and flight endurance of the five-rotor UAV. Genetic algorithm (GA) optimization is used to specify the parameters of the disturbance-observer-based TSMC (GATSMC) to decrease chattering. Finally, the superior performance of FTSMC is investigated over TSMC and GATSMC.
doi_str_mv 10.1016/j.apm.2019.01.010
format Article
fullrecord <record><control><sourceid>proquest_cross</sourceid><recordid>TN_cdi_proquest_journals_2232661596</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><els_id>S0307904X19300289</els_id><sourcerecordid>2232661596</sourcerecordid><originalsourceid>FETCH-LOGICAL-c368t-ddc3e3c03e808b2cdaf64ee6f9afbefcf16b5a98ac8d98b02d05969a9743801c3</originalsourceid><addsrcrecordid>eNp9UE1LAzEUDKJgrf4AbwHPu75s2nQXT1K_Ci29KHgL2eRFUnY3NdkttL_elHrwJDx478HMMDOE3DLIGTBxv8nVts0LYFUOLA2ckRFwmGUVTD7P_9yX5CrGDQBM0zci-snFfgi16jRmvo4YdhiyWkU01A6Hw572GFrXqYbGxhnXfdHWG6Tad33wDbU-0NVitaZDEgi9ch3tfNe4DlWgcR97bOM1ubCqiXjzu8fk4-X5ff6WLdevi_njMtNclH1mjObINXAsoawLbZQVE0RhK2VrtNoyUU9VVSpdmqqsoTApg6hUNZvwEpjmY3J30t0G_z1g7OXGDyFZj7IoeCEES_iEYieUDj7GgFZug2tV2EsG8til3MjUpTx2KYGlgcR5OHEw2d85DDJqhymxcQF1L413_7B_APcEfxk</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>2232661596</pqid></control><display><type>article</type><title>Disturbance-observer-based fuzzy terminal sliding mode control for MIMO uncertain nonlinear systems</title><source>Elsevier ScienceDirect Journals</source><source>Elektronische Zeitschriftenbibliothek - Frei zugängliche E-Journals</source><source>Business Source Complete</source><source>Education Source</source><creator>Vahidi-Moghaddam, Amin ; Rajaei, Arman ; Ayati, Moosa</creator><creatorcontrib>Vahidi-Moghaddam, Amin ; Rajaei, Arman ; Ayati, Moosa</creatorcontrib><description>•Modelling and simulation of a novel five-rotor unmanned aerial vehicle with an extra rotor.•Proposing a disturbance-observer-based fuzzy terminal sliding mode controller.•Considering MIMO uncertain nonlinear systems with unmeasured external disturbance.•Unknown non-symmetric input saturation and control singularity are investigated.•Closed-loop stability and convergence of the state estimations in finite time are proved. This study is concerned with the design of a disturbance-observer-based fuzzy terminal sliding mode controller (FTSMC) for multi-input multi-output (MIMO) uncertain nonlinear systems by considering unknown non-symmetric input saturation and control singularity. The disturbance observer is proposed for the unmeasured external disturbance and guarantees the convergence of the disturbance estimation error to zero in a finite time. The terminal sliding mode controller (TSMC) is designed for MIMO uncertain nonlinear systems by utilizing the output of the proposed disturbance observer. This control scheme combines the disturbance-observer-based TSMC with a fuzzy logic system in the presence of unknown non-symmetric input saturation and control singularity in order to reduce chattering phenomena. Finite time asymptotic stability, convergence of the disturbance observer, and convergence of the closed-loop system are proved via Lyapunov stability theorem. In addition, a five-rotor unmanned aerial vehicle (UAV) is employed in the numerical simulations to demonstrate the effectiveness and performance of the proposed control scheme. Disturbance observer estimates the payload and flight endurance of the five-rotor UAV. Genetic algorithm (GA) optimization is used to specify the parameters of the disturbance-observer-based TSMC (GATSMC) to decrease chattering. Finally, the superior performance of FTSMC is investigated over TSMC and GATSMC.</description><identifier>ISSN: 0307-904X</identifier><identifier>ISSN: 1088-8691</identifier><identifier>EISSN: 0307-904X</identifier><identifier>DOI: 10.1016/j.apm.2019.01.010</identifier><language>eng</language><publisher>New York: Elsevier Inc</publisher><subject>Computer simulation ; Control stability ; Control systems design ; Controllers ; Convergence ; Disturbance observer ; Disturbance observers ; Endurance ; Feedback control ; Five-rotor unmanned aerial vehicle ; Fuzzy control ; Fuzzy logic ; Fuzzy systems ; Fuzzy terminal sliding mode control ; Genetic algorithms ; MIMO (control systems) ; MIMO uncertain nonlinear systems ; Non- symmetric input saturation ; Nonlinear control ; Nonlinear systems ; Optimization ; Saturation ; Sliding mode control ; Unmanned aerial vehicles</subject><ispartof>Applied Mathematical Modelling, 2019-06, Vol.70, p.109-127</ispartof><rights>2019 Elsevier Inc.</rights><rights>Copyright Elsevier BV Jun 2019</rights><lds50>peer_reviewed</lds50><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c368t-ddc3e3c03e808b2cdaf64ee6f9afbefcf16b5a98ac8d98b02d05969a9743801c3</citedby><cites>FETCH-LOGICAL-c368t-ddc3e3c03e808b2cdaf64ee6f9afbefcf16b5a98ac8d98b02d05969a9743801c3</cites><orcidid>0000-0001-9943-739X</orcidid></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://dx.doi.org/10.1016/j.apm.2019.01.010$$EHTML$$P50$$Gelsevier$$H</linktohtml><link.rule.ids>314,777,781,3537,27905,27906,45976</link.rule.ids></links><search><creatorcontrib>Vahidi-Moghaddam, Amin</creatorcontrib><creatorcontrib>Rajaei, Arman</creatorcontrib><creatorcontrib>Ayati, Moosa</creatorcontrib><title>Disturbance-observer-based fuzzy terminal sliding mode control for MIMO uncertain nonlinear systems</title><title>Applied Mathematical Modelling</title><description>•Modelling and simulation of a novel five-rotor unmanned aerial vehicle with an extra rotor.•Proposing a disturbance-observer-based fuzzy terminal sliding mode controller.•Considering MIMO uncertain nonlinear systems with unmeasured external disturbance.•Unknown non-symmetric input saturation and control singularity are investigated.•Closed-loop stability and convergence of the state estimations in finite time are proved. This study is concerned with the design of a disturbance-observer-based fuzzy terminal sliding mode controller (FTSMC) for multi-input multi-output (MIMO) uncertain nonlinear systems by considering unknown non-symmetric input saturation and control singularity. The disturbance observer is proposed for the unmeasured external disturbance and guarantees the convergence of the disturbance estimation error to zero in a finite time. The terminal sliding mode controller (TSMC) is designed for MIMO uncertain nonlinear systems by utilizing the output of the proposed disturbance observer. This control scheme combines the disturbance-observer-based TSMC with a fuzzy logic system in the presence of unknown non-symmetric input saturation and control singularity in order to reduce chattering phenomena. Finite time asymptotic stability, convergence of the disturbance observer, and convergence of the closed-loop system are proved via Lyapunov stability theorem. In addition, a five-rotor unmanned aerial vehicle (UAV) is employed in the numerical simulations to demonstrate the effectiveness and performance of the proposed control scheme. Disturbance observer estimates the payload and flight endurance of the five-rotor UAV. Genetic algorithm (GA) optimization is used to specify the parameters of the disturbance-observer-based TSMC (GATSMC) to decrease chattering. Finally, the superior performance of FTSMC is investigated over TSMC and GATSMC.</description><subject>Computer simulation</subject><subject>Control stability</subject><subject>Control systems design</subject><subject>Controllers</subject><subject>Convergence</subject><subject>Disturbance observer</subject><subject>Disturbance observers</subject><subject>Endurance</subject><subject>Feedback control</subject><subject>Five-rotor unmanned aerial vehicle</subject><subject>Fuzzy control</subject><subject>Fuzzy logic</subject><subject>Fuzzy systems</subject><subject>Fuzzy terminal sliding mode control</subject><subject>Genetic algorithms</subject><subject>MIMO (control systems)</subject><subject>MIMO uncertain nonlinear systems</subject><subject>Non- symmetric input saturation</subject><subject>Nonlinear control</subject><subject>Nonlinear systems</subject><subject>Optimization</subject><subject>Saturation</subject><subject>Sliding mode control</subject><subject>Unmanned aerial vehicles</subject><issn>0307-904X</issn><issn>1088-8691</issn><issn>0307-904X</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2019</creationdate><recordtype>article</recordtype><recordid>eNp9UE1LAzEUDKJgrf4AbwHPu75s2nQXT1K_Ci29KHgL2eRFUnY3NdkttL_elHrwJDx478HMMDOE3DLIGTBxv8nVts0LYFUOLA2ckRFwmGUVTD7P_9yX5CrGDQBM0zci-snFfgi16jRmvo4YdhiyWkU01A6Hw572GFrXqYbGxhnXfdHWG6Tad33wDbU-0NVitaZDEgi9ch3tfNe4DlWgcR97bOM1ubCqiXjzu8fk4-X5ff6WLdevi_njMtNclH1mjObINXAsoawLbZQVE0RhK2VrtNoyUU9VVSpdmqqsoTApg6hUNZvwEpjmY3J30t0G_z1g7OXGDyFZj7IoeCEES_iEYieUDj7GgFZug2tV2EsG8til3MjUpTx2KYGlgcR5OHEw2d85DDJqhymxcQF1L413_7B_APcEfxk</recordid><startdate>201906</startdate><enddate>201906</enddate><creator>Vahidi-Moghaddam, Amin</creator><creator>Rajaei, Arman</creator><creator>Ayati, Moosa</creator><general>Elsevier Inc</general><general>Elsevier BV</general><scope>AAYXX</scope><scope>CITATION</scope><scope>7SC</scope><scope>8FD</scope><scope>JQ2</scope><scope>L7M</scope><scope>L~C</scope><scope>L~D</scope><orcidid>https://orcid.org/0000-0001-9943-739X</orcidid></search><sort><creationdate>201906</creationdate><title>Disturbance-observer-based fuzzy terminal sliding mode control for MIMO uncertain nonlinear systems</title><author>Vahidi-Moghaddam, Amin ; Rajaei, Arman ; Ayati, Moosa</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c368t-ddc3e3c03e808b2cdaf64ee6f9afbefcf16b5a98ac8d98b02d05969a9743801c3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2019</creationdate><topic>Computer simulation</topic><topic>Control stability</topic><topic>Control systems design</topic><topic>Controllers</topic><topic>Convergence</topic><topic>Disturbance observer</topic><topic>Disturbance observers</topic><topic>Endurance</topic><topic>Feedback control</topic><topic>Five-rotor unmanned aerial vehicle</topic><topic>Fuzzy control</topic><topic>Fuzzy logic</topic><topic>Fuzzy systems</topic><topic>Fuzzy terminal sliding mode control</topic><topic>Genetic algorithms</topic><topic>MIMO (control systems)</topic><topic>MIMO uncertain nonlinear systems</topic><topic>Non- symmetric input saturation</topic><topic>Nonlinear control</topic><topic>Nonlinear systems</topic><topic>Optimization</topic><topic>Saturation</topic><topic>Sliding mode control</topic><topic>Unmanned aerial vehicles</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Vahidi-Moghaddam, Amin</creatorcontrib><creatorcontrib>Rajaei, Arman</creatorcontrib><creatorcontrib>Ayati, Moosa</creatorcontrib><collection>CrossRef</collection><collection>Computer and Information Systems Abstracts</collection><collection>Technology Research Database</collection><collection>ProQuest Computer Science Collection</collection><collection>Advanced Technologies Database with Aerospace</collection><collection>Computer and Information Systems Abstracts – Academic</collection><collection>Computer and Information Systems Abstracts Professional</collection><jtitle>Applied Mathematical Modelling</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Vahidi-Moghaddam, Amin</au><au>Rajaei, Arman</au><au>Ayati, Moosa</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Disturbance-observer-based fuzzy terminal sliding mode control for MIMO uncertain nonlinear systems</atitle><jtitle>Applied Mathematical Modelling</jtitle><date>2019-06</date><risdate>2019</risdate><volume>70</volume><spage>109</spage><epage>127</epage><pages>109-127</pages><issn>0307-904X</issn><issn>1088-8691</issn><eissn>0307-904X</eissn><abstract>•Modelling and simulation of a novel five-rotor unmanned aerial vehicle with an extra rotor.•Proposing a disturbance-observer-based fuzzy terminal sliding mode controller.•Considering MIMO uncertain nonlinear systems with unmeasured external disturbance.•Unknown non-symmetric input saturation and control singularity are investigated.•Closed-loop stability and convergence of the state estimations in finite time are proved. This study is concerned with the design of a disturbance-observer-based fuzzy terminal sliding mode controller (FTSMC) for multi-input multi-output (MIMO) uncertain nonlinear systems by considering unknown non-symmetric input saturation and control singularity. The disturbance observer is proposed for the unmeasured external disturbance and guarantees the convergence of the disturbance estimation error to zero in a finite time. The terminal sliding mode controller (TSMC) is designed for MIMO uncertain nonlinear systems by utilizing the output of the proposed disturbance observer. This control scheme combines the disturbance-observer-based TSMC with a fuzzy logic system in the presence of unknown non-symmetric input saturation and control singularity in order to reduce chattering phenomena. Finite time asymptotic stability, convergence of the disturbance observer, and convergence of the closed-loop system are proved via Lyapunov stability theorem. In addition, a five-rotor unmanned aerial vehicle (UAV) is employed in the numerical simulations to demonstrate the effectiveness and performance of the proposed control scheme. Disturbance observer estimates the payload and flight endurance of the five-rotor UAV. Genetic algorithm (GA) optimization is used to specify the parameters of the disturbance-observer-based TSMC (GATSMC) to decrease chattering. Finally, the superior performance of FTSMC is investigated over TSMC and GATSMC.</abstract><cop>New York</cop><pub>Elsevier Inc</pub><doi>10.1016/j.apm.2019.01.010</doi><tpages>19</tpages><orcidid>https://orcid.org/0000-0001-9943-739X</orcidid><oa>free_for_read</oa></addata></record>
fulltext fulltext
identifier ISSN: 0307-904X
ispartof Applied Mathematical Modelling, 2019-06, Vol.70, p.109-127
issn 0307-904X
1088-8691
0307-904X
language eng
recordid cdi_proquest_journals_2232661596
source Elsevier ScienceDirect Journals; Elektronische Zeitschriftenbibliothek - Frei zugängliche E-Journals; Business Source Complete; Education Source
subjects Computer simulation
Control stability
Control systems design
Controllers
Convergence
Disturbance observer
Disturbance observers
Endurance
Feedback control
Five-rotor unmanned aerial vehicle
Fuzzy control
Fuzzy logic
Fuzzy systems
Fuzzy terminal sliding mode control
Genetic algorithms
MIMO (control systems)
MIMO uncertain nonlinear systems
Non- symmetric input saturation
Nonlinear control
Nonlinear systems
Optimization
Saturation
Sliding mode control
Unmanned aerial vehicles
title Disturbance-observer-based fuzzy terminal sliding mode control for MIMO uncertain nonlinear systems
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-20T00%3A19%3A58IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-proquest_cross&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.genre=article&rft.atitle=Disturbance-observer-based%20fuzzy%20terminal%20sliding%20mode%20control%20for%20MIMO%20uncertain%20nonlinear%20systems&rft.jtitle=Applied%20Mathematical%20Modelling&rft.au=Vahidi-Moghaddam,%20Amin&rft.date=2019-06&rft.volume=70&rft.spage=109&rft.epage=127&rft.pages=109-127&rft.issn=0307-904X&rft.eissn=0307-904X&rft_id=info:doi/10.1016/j.apm.2019.01.010&rft_dat=%3Cproquest_cross%3E2232661596%3C/proquest_cross%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_pqid=2232661596&rft_id=info:pmid/&rft_els_id=S0307904X19300289&rfr_iscdi=true