Quasi-continuous higher-order sliding mode controller designs for spacecraft attitude tracking manoeuvres
This paper studies high-order sliding mode control laws to deal with some spacecraft attitude tracking problems. Second and third order quasi-continuous sliding control are applied to quaternion-based spacecraft attitude tracking manoeuvres. A class of linear sliding manifolds is selected as a funct...
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| creator | Pukdeboon, C. Zinober, A.S.I. Thein, M.-W.L. |
| description | This paper studies high-order sliding mode control laws to deal with some spacecraft attitude tracking problems. Second and third order quasi-continuous sliding control are applied to quaternion-based spacecraft attitude tracking manoeuvres. A class of linear sliding manifolds is selected as a function of angular velocities and quaternion errors. The second method of Lyapunov theory is used to show that tracking is achieved globally. An example of multiaxial attitude tracking manoeuvres is presented and simulation results are included to verify and compare the usefulness of the various controllers. |
| doi_str_mv | 10.1109/VSS.2008.4570710 |
| format | Conference Proceeding |
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Second and third order quasi-continuous sliding control are applied to quaternion-based spacecraft attitude tracking manoeuvres. A class of linear sliding manifolds is selected as a function of angular velocities and quaternion errors. The second method of Lyapunov theory is used to show that tracking is achieved globally. 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Second and third order quasi-continuous sliding control are applied to quaternion-based spacecraft attitude tracking manoeuvres. A class of linear sliding manifolds is selected as a function of angular velocities and quaternion errors. The second method of Lyapunov theory is used to show that tracking is achieved globally. An example of multiaxial attitude tracking manoeuvres is presented and simulation results are included to verify and compare the usefulness of the various controllers.</description><subject>Angular velocity</subject><subject>Angular velocity control</subject><subject>Attitude control</subject><subject>Kinematics</subject><subject>Mathematics</subject><subject>Mechanical engineering</subject><subject>Nonlinear equations</subject><subject>Quaternions</subject><subject>Sliding mode control</subject><subject>Space vehicles</subject><issn>2158-3978</issn><isbn>1424421993</isbn><isbn>9781424421992</isbn><isbn>1424422000</isbn><isbn>9781424422005</isbn><fulltext>true</fulltext><rsrctype>conference_proceeding</rsrctype><creationdate>2008</creationdate><recordtype>conference_proceeding</recordtype><sourceid>6IE</sourceid><sourceid>RIE</sourceid><recordid>eNo1kEtLAzEUhSNasK3dC27mD0zNTdI8llJ8QUGk6rZkJkkbnU5KkhH896Y-Vod7-M6BcxG6BDwHwOr6bb2eE4zlnC0EFoBP0AQYYYwUE5_-H6AUPUNjAgtZUyXkCE2OIYWBAjtHs5TeC05BKmAwRv550MnXbeiz74cwpGrntzsb6xCNjVXqvPH9ttoHY6sjFEPXFd_Y5Ld9qlwozEG3to3a5Urn7PNQ0Bx1-_ET1H2ww2e06QKNnO6Snf3pFL3e3b4sH-rV0_3j8mZVewIi11S4BiTHzJY1uOUSGuMIZrQBzrTDxhlRxiisF9w5xbR0vMGGcsldI4igU3T12-uttZtD9HsdvzZ_P6Pf7_NdrQ</recordid><startdate>20080101</startdate><enddate>20080101</enddate><creator>Pukdeboon, C.</creator><creator>Zinober, A.S.I.</creator><creator>Thein, M.-W.L.</creator><general>IEEE</general><scope>6IE</scope><scope>6IL</scope><scope>CBEJK</scope><scope>RIE</scope><scope>RIL</scope></search><sort><creationdate>20080101</creationdate><title>Quasi-continuous higher-order sliding mode controller designs for spacecraft attitude tracking manoeuvres</title><author>Pukdeboon, C. ; Zinober, A.S.I. ; Thein, M.-W.L.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-i217t-37fb18604e2440c681bdf2043b164af0dfd790190a56ff94a8f6b0d3686fb7273</frbrgroupid><rsrctype>conference_proceedings</rsrctype><prefilter>conference_proceedings</prefilter><language>eng</language><creationdate>2008</creationdate><topic>Angular velocity</topic><topic>Angular velocity control</topic><topic>Attitude control</topic><topic>Kinematics</topic><topic>Mathematics</topic><topic>Mechanical engineering</topic><topic>Nonlinear equations</topic><topic>Quaternions</topic><topic>Sliding mode control</topic><topic>Space vehicles</topic><toplevel>online_resources</toplevel><creatorcontrib>Pukdeboon, C.</creatorcontrib><creatorcontrib>Zinober, A.S.I.</creatorcontrib><creatorcontrib>Thein, M.-W.L.</creatorcontrib><collection>IEEE Electronic Library (IEL) Conference Proceedings</collection><collection>IEEE Proceedings Order Plan All Online (POP All Online) 1998-present by volume</collection><collection>IEEE Xplore All Conference Proceedings</collection><collection>IEEE Electronic Library (IEL)</collection><collection>IEEE Proceedings Order Plans (POP All) 1998-Present</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Pukdeboon, C.</au><au>Zinober, A.S.I.</au><au>Thein, M.-W.L.</au><format>book</format><genre>proceeding</genre><ristype>CONF</ristype><atitle>Quasi-continuous higher-order sliding mode controller designs for spacecraft attitude tracking manoeuvres</atitle><btitle>2008 International Workshop on Variable Structure Systems</btitle><stitle>VSS</stitle><date>2008-01-01</date><risdate>2008</risdate><spage>215</spage><epage>220</epage><pages>215-220</pages><issn>2158-3978</issn><isbn>1424421993</isbn><isbn>9781424421992</isbn><eisbn>1424422000</eisbn><eisbn>9781424422005</eisbn><abstract>This paper studies high-order sliding mode control laws to deal with some spacecraft attitude tracking problems. Second and third order quasi-continuous sliding control are applied to quaternion-based spacecraft attitude tracking manoeuvres. A class of linear sliding manifolds is selected as a function of angular velocities and quaternion errors. The second method of Lyapunov theory is used to show that tracking is achieved globally. An example of multiaxial attitude tracking manoeuvres is presented and simulation results are included to verify and compare the usefulness of the various controllers.</abstract><pub>IEEE</pub><doi>10.1109/VSS.2008.4570710</doi><tpages>6</tpages><oa>free_for_read</oa></addata></record> |
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| issn | 2158-3978 |
| language | eng |
| recordid | cdi_ieee_primary_4570710 |
| source | IEEE Electronic Library (IEL) Conference Proceedings |
| subjects | Angular velocity Angular velocity control Attitude control Kinematics Mathematics Mechanical engineering Nonlinear equations Quaternions Sliding mode control Space vehicles |
| title | Quasi-continuous higher-order sliding mode controller designs for spacecraft attitude tracking manoeuvres |
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