Fuzzy Disturbance Observer Based Fixed-time Sliding Mode Control for Hypersonic Morphing Vehicles with Uncertainties
This work focuses on the attitude control problem for hypersonic morphing vehicles(HMVs) with uncertainties. A span-morphing HMV model is firstly established with lumped disturbances. Based on fixed-time technique, a disturbance observer with fuzzy logic system(FLS) is proposed to enhance the robust...
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| Veröffentlicht in: | IEEE transactions on aerospace and electronic systems 2023-08, Vol.59 (4), p.1-10 |
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| creator | Chen, Haolan Wang, Peng Tang, Guojian |
| description | This work focuses on the attitude control problem for hypersonic morphing vehicles(HMVs) with uncertainties. A span-morphing HMV model is firstly established with lumped disturbances. Based on fixed-time technique, a disturbance observer with fuzzy logic system(FLS) is proposed to enhance the robustness by estimating the unmodelled dynamics and external disturbances in fixed settling time. The multivariable fixed-time sliding mode manifold is applied to the transformed control system, which guarantees a direct control input design from attitude command and decent tracking performance. Then, the control system degenerates into an autonomous system, and the closed-loop fixed-time stability is ensured via Lyapunov synthesis and homogeneity theory. Finally, simulation results are presented to demonstrate the effectiveness of the proposed control scheme. |
| doi_str_mv | 10.1109/TAES.2022.3227886 |
| format | Article |
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A span-morphing HMV model is firstly established with lumped disturbances. Based on fixed-time technique, a disturbance observer with fuzzy logic system(FLS) is proposed to enhance the robustness by estimating the unmodelled dynamics and external disturbances in fixed settling time. The multivariable fixed-time sliding mode manifold is applied to the transformed control system, which guarantees a direct control input design from attitude command and decent tracking performance. Then, the control system degenerates into an autonomous system, and the closed-loop fixed-time stability is ensured via Lyapunov synthesis and homogeneity theory. Finally, simulation results are presented to demonstrate the effectiveness of the proposed control scheme.</description><identifier>ISSN: 0018-9251</identifier><identifier>EISSN: 1557-9603</identifier><identifier>DOI: 10.1109/TAES.2022.3227886</identifier><identifier>CODEN: IEARAX</identifier><language>eng</language><publisher>New York: IEEE</publisher><subject>Aerodynamics ; Attitude control ; Closed loops ; Control systems ; Convergence ; Disturbance observers ; fixed-time stability ; Fuzzy disturbance observer (FDO) ; Fuzzy logic ; Homogeneity ; homogeneity theory ; hypersonic morphing vehicles (HMVs) ; Morphing ; Multivariable control ; Robustness (mathematics) ; Sliding mode control ; sliding mode control (SMC) ; Stability criteria ; Tracking control ; Uncertainty ; Vehicle dynamics</subject><ispartof>IEEE transactions on aerospace and electronic systems, 2023-08, Vol.59 (4), p.1-10</ispartof><rights>Copyright The Institute of Electrical and Electronics Engineers, Inc. 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A span-morphing HMV model is firstly established with lumped disturbances. Based on fixed-time technique, a disturbance observer with fuzzy logic system(FLS) is proposed to enhance the robustness by estimating the unmodelled dynamics and external disturbances in fixed settling time. The multivariable fixed-time sliding mode manifold is applied to the transformed control system, which guarantees a direct control input design from attitude command and decent tracking performance. Then, the control system degenerates into an autonomous system, and the closed-loop fixed-time stability is ensured via Lyapunov synthesis and homogeneity theory. Finally, simulation results are presented to demonstrate the effectiveness of the proposed control scheme.</description><subject>Aerodynamics</subject><subject>Attitude control</subject><subject>Closed loops</subject><subject>Control systems</subject><subject>Convergence</subject><subject>Disturbance observers</subject><subject>fixed-time stability</subject><subject>Fuzzy disturbance observer (FDO)</subject><subject>Fuzzy logic</subject><subject>Homogeneity</subject><subject>homogeneity theory</subject><subject>hypersonic morphing vehicles (HMVs)</subject><subject>Morphing</subject><subject>Multivariable control</subject><subject>Robustness (mathematics)</subject><subject>Sliding mode control</subject><subject>sliding mode control (SMC)</subject><subject>Stability criteria</subject><subject>Tracking control</subject><subject>Uncertainty</subject><subject>Vehicle dynamics</subject><issn>0018-9251</issn><issn>1557-9603</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2023</creationdate><recordtype>article</recordtype><sourceid>RIE</sourceid><recordid>eNpNkE1PwjAYxxujiYh-ABMPTTwP-7Kt3RERxATDAfC6dO0zKRkbtp0Kn94ROHh68s_zf0l-CN1TMqCUZE_L4XgxYISxAWdMSJleoB5NEhFlKeGXqEcIlVHGEnqNbrzfdDKWMe-hMGkPhz1-sT60rlC1BjwvPLhvcPhZeTB4Yn_BRMFuAS8qa2z9id8bA3jU1ME1FS4bh6f7HTjf1FZ3P7dbH00fsLa6Ao9_bFjjVdfsgrJ1sOBv0VWpKg9359tHq8l4OZpGs_nr22g4izTL4hAZrRkYrokwQlLGSKIMZ7EoE56YTIqyEERyxRJeFkYqVvBSGyVFWhjWSeB99Hjq3bnmqwUf8k3TurqbzJmMRZYmogv3ET25tGu8d1DmO2e3yu1zSvIj3PwINz_Czc9wu8zDKWMB4J-fxHGaSv4Hutd31Q</recordid><startdate>20230801</startdate><enddate>20230801</enddate><creator>Chen, Haolan</creator><creator>Wang, Peng</creator><creator>Tang, Guojian</creator><general>IEEE</general><general>The Institute of Electrical and Electronics Engineers, Inc. (IEEE)</general><scope>97E</scope><scope>RIA</scope><scope>RIE</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>7SP</scope><scope>7TB</scope><scope>8FD</scope><scope>FR3</scope><scope>H8D</scope><scope>L7M</scope><orcidid>https://orcid.org/0000-0001-5463-9895</orcidid><orcidid>https://orcid.org/0000-0003-0043-1487</orcidid><orcidid>https://orcid.org/0000-0001-5198-5477</orcidid></search><sort><creationdate>20230801</creationdate><title>Fuzzy Disturbance Observer Based Fixed-time Sliding Mode Control for Hypersonic Morphing Vehicles with Uncertainties</title><author>Chen, Haolan ; Wang, Peng ; Tang, Guojian</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c294t-dcc2ed3c07d7812205ad3247f535d987fb7083a253fbd8a2b3fcda876bd28a2e3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2023</creationdate><topic>Aerodynamics</topic><topic>Attitude control</topic><topic>Closed loops</topic><topic>Control systems</topic><topic>Convergence</topic><topic>Disturbance observers</topic><topic>fixed-time stability</topic><topic>Fuzzy disturbance observer (FDO)</topic><topic>Fuzzy logic</topic><topic>Homogeneity</topic><topic>homogeneity theory</topic><topic>hypersonic morphing vehicles (HMVs)</topic><topic>Morphing</topic><topic>Multivariable control</topic><topic>Robustness (mathematics)</topic><topic>Sliding mode control</topic><topic>sliding mode control (SMC)</topic><topic>Stability criteria</topic><topic>Tracking control</topic><topic>Uncertainty</topic><topic>Vehicle dynamics</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Chen, Haolan</creatorcontrib><creatorcontrib>Wang, Peng</creatorcontrib><creatorcontrib>Tang, Guojian</creatorcontrib><collection>IEEE All-Society Periodicals Package (ASPP) 2005-present</collection><collection>IEEE All-Society Periodicals Package (ASPP) 1998-Present</collection><collection>IEEE Electronic Library (IEL)</collection><collection>CrossRef</collection><collection>Electronics & Communications Abstracts</collection><collection>Mechanical & Transportation Engineering Abstracts</collection><collection>Technology Research Database</collection><collection>Engineering Research Database</collection><collection>Aerospace Database</collection><collection>Advanced Technologies Database with Aerospace</collection><jtitle>IEEE transactions on aerospace and electronic systems</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Chen, Haolan</au><au>Wang, Peng</au><au>Tang, Guojian</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Fuzzy Disturbance Observer Based Fixed-time Sliding Mode Control for Hypersonic Morphing Vehicles with Uncertainties</atitle><jtitle>IEEE transactions on aerospace and electronic systems</jtitle><stitle>T-AES</stitle><date>2023-08-01</date><risdate>2023</risdate><volume>59</volume><issue>4</issue><spage>1</spage><epage>10</epage><pages>1-10</pages><issn>0018-9251</issn><eissn>1557-9603</eissn><coden>IEARAX</coden><abstract>This work focuses on the attitude control problem for hypersonic morphing vehicles(HMVs) with uncertainties. A span-morphing HMV model is firstly established with lumped disturbances. Based on fixed-time technique, a disturbance observer with fuzzy logic system(FLS) is proposed to enhance the robustness by estimating the unmodelled dynamics and external disturbances in fixed settling time. The multivariable fixed-time sliding mode manifold is applied to the transformed control system, which guarantees a direct control input design from attitude command and decent tracking performance. Then, the control system degenerates into an autonomous system, and the closed-loop fixed-time stability is ensured via Lyapunov synthesis and homogeneity theory. 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| source | IEEE Electronic Library (IEL) |
| subjects | Aerodynamics Attitude control Closed loops Control systems Convergence Disturbance observers fixed-time stability Fuzzy disturbance observer (FDO) Fuzzy logic Homogeneity homogeneity theory hypersonic morphing vehicles (HMVs) Morphing Multivariable control Robustness (mathematics) Sliding mode control sliding mode control (SMC) Stability criteria Tracking control Uncertainty Vehicle dynamics |
| title | Fuzzy Disturbance Observer Based Fixed-time Sliding Mode Control for Hypersonic Morphing Vehicles with Uncertainties |
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