Robust dynamic surface sliding mode control for attitude tracking of flexible spacecraft with an extended state observer
The nonlinear attitude motion equations of flexible spacecraft described by the Euler angles are expressed in the vector form. Based on dynamic surface control, a new robust dynamic surface sliding mode controller is proposed for the attitude tracking and active vibration suppression of flexible spa...
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| Veröffentlicht in: | Proceedings of the Institution of Mechanical Engineers. Part G, Journal of aerospace engineering Journal of aerospace engineering, 2017-03, Vol.231 (3), p.533-547 |
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| container_title | Proceedings of the Institution of Mechanical Engineers. Part G, Journal of aerospace engineering |
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| creator | Zhou, Chengbao Zhou, Di |
| description | The nonlinear attitude motion equations of flexible spacecraft described by the Euler angles are expressed in the vector form. Based on dynamic surface control, a new robust dynamic surface sliding mode controller is proposed for the attitude tracking and active vibration suppression of flexible spacecraft in the presence of parameter uncertainty and external disturbances. Then, a novel robust dynamic surface finite time sliding mode controller is proposed with an extended state observer such that the uncertainties can be estimated. Lyapunov stability analyses show that the two controllers can guarantee the asymptotical stability of the attitude control system. The undesirable vibration of flexible spacecraft is also actively suppressed by the modal velocity feedback approach. Finally, simulation results verified the effectiveness of the presented control algorithms. |
| doi_str_mv | 10.1177/0954410016640822 |
| format | Article |
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Based on dynamic surface control, a new robust dynamic surface sliding mode controller is proposed for the attitude tracking and active vibration suppression of flexible spacecraft in the presence of parameter uncertainty and external disturbances. Then, a novel robust dynamic surface finite time sliding mode controller is proposed with an extended state observer such that the uncertainties can be estimated. Lyapunov stability analyses show that the two controllers can guarantee the asymptotical stability of the attitude control system. The undesirable vibration of flexible spacecraft is also actively suppressed by the modal velocity feedback approach. Finally, simulation results verified the effectiveness of the presented control algorithms.</description><identifier>ISSN: 0954-4100</identifier><identifier>EISSN: 2041-3025</identifier><identifier>DOI: 10.1177/0954410016640822</identifier><language>eng</language><publisher>London, England: SAGE Publications</publisher><subject>Algorithms ; Attitude stability ; Computer simulation ; Control algorithms ; Control stability ; Controllers ; Equations of motion ; Euler angles ; Flexible spacecraft ; Nonlinear equations ; Parameter uncertainty ; Robust control ; Sliding mode control ; Spacecraft ; Spacecraft attitude control ; Spacecraft stability ; Spacecraft tracking ; Stability analysis ; State observers ; Tracking control ; Vibration control</subject><ispartof>Proceedings of the Institution of Mechanical Engineers. 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Finally, simulation results verified the effectiveness of the presented control algorithms.</description><subject>Algorithms</subject><subject>Attitude stability</subject><subject>Computer simulation</subject><subject>Control algorithms</subject><subject>Control stability</subject><subject>Controllers</subject><subject>Equations of motion</subject><subject>Euler angles</subject><subject>Flexible spacecraft</subject><subject>Nonlinear equations</subject><subject>Parameter uncertainty</subject><subject>Robust control</subject><subject>Sliding mode control</subject><subject>Spacecraft</subject><subject>Spacecraft attitude control</subject><subject>Spacecraft stability</subject><subject>Spacecraft tracking</subject><subject>Stability analysis</subject><subject>State observers</subject><subject>Tracking control</subject><subject>Vibration control</subject><issn>0954-4100</issn><issn>2041-3025</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2017</creationdate><recordtype>article</recordtype><recordid>eNp1kM1LxDAQxYMouH7cPQY8V5M0_chRFr9gQRA9l2kyWbt2mzVJdfe_N2UFQXAuA_N-7w08Qi44u-K8qq6ZKqTkjPGylKwW4oDMBJM8y5koDslskrNJPyYnIaxYmqLMZ2T77NoxRGp2A6w7TcPoLWikoe9MNyzp2hmk2g3Ru55a5ynE2MUxHaMH_T4hzlLb47Zr-2TbJLP2YCP96uIbhYHiNuJg0NAQISJ1bUD_if6MHFnoA57_7FPyenf7Mn_IFk_3j_ObRaZzpmJmhK4ZAlfCSl2VhTK2bEuGVoGodFUbQFDY5hal1a0SwnBR5yArYFIaq_NTcrnP3Xj3MWKIzcqNfkgvGyGFVKkkKRLF9pT2LgSPttn4bg1-13DWTP02f_tNlmxvCbDE39B_-W-02Hzz</recordid><startdate>201703</startdate><enddate>201703</enddate><creator>Zhou, Chengbao</creator><creator>Zhou, Di</creator><general>SAGE Publications</general><general>SAGE PUBLICATIONS, INC</general><scope>AAYXX</scope><scope>CITATION</scope><scope>7TB</scope><scope>8FD</scope><scope>F28</scope><scope>FR3</scope><scope>H8D</scope><scope>L7M</scope></search><sort><creationdate>201703</creationdate><title>Robust dynamic surface sliding mode control for attitude tracking of flexible spacecraft with an extended state observer</title><author>Zhou, Chengbao ; Zhou, Di</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c309t-d2c80ea192f4c7659df6b60ef9a27c78daea9eb3fe4fcb922d1283a47a044dfc3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2017</creationdate><topic>Algorithms</topic><topic>Attitude stability</topic><topic>Computer simulation</topic><topic>Control algorithms</topic><topic>Control stability</topic><topic>Controllers</topic><topic>Equations of motion</topic><topic>Euler angles</topic><topic>Flexible spacecraft</topic><topic>Nonlinear equations</topic><topic>Parameter uncertainty</topic><topic>Robust control</topic><topic>Sliding mode control</topic><topic>Spacecraft</topic><topic>Spacecraft attitude control</topic><topic>Spacecraft stability</topic><topic>Spacecraft tracking</topic><topic>Stability analysis</topic><topic>State observers</topic><topic>Tracking control</topic><topic>Vibration control</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Zhou, Chengbao</creatorcontrib><creatorcontrib>Zhou, Di</creatorcontrib><collection>CrossRef</collection><collection>Mechanical & Transportation Engineering Abstracts</collection><collection>Technology Research Database</collection><collection>ANTE: Abstracts in New Technology & Engineering</collection><collection>Engineering Research Database</collection><collection>Aerospace Database</collection><collection>Advanced Technologies Database with Aerospace</collection><jtitle>Proceedings of the Institution of Mechanical Engineers. 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Based on dynamic surface control, a new robust dynamic surface sliding mode controller is proposed for the attitude tracking and active vibration suppression of flexible spacecraft in the presence of parameter uncertainty and external disturbances. Then, a novel robust dynamic surface finite time sliding mode controller is proposed with an extended state observer such that the uncertainties can be estimated. Lyapunov stability analyses show that the two controllers can guarantee the asymptotical stability of the attitude control system. The undesirable vibration of flexible spacecraft is also actively suppressed by the modal velocity feedback approach. Finally, simulation results verified the effectiveness of the presented control algorithms.</abstract><cop>London, England</cop><pub>SAGE Publications</pub><doi>10.1177/0954410016640822</doi><tpages>15</tpages></addata></record> |
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| identifier | ISSN: 0954-4100 |
| ispartof | Proceedings of the Institution of Mechanical Engineers. Part G, Journal of aerospace engineering, 2017-03, Vol.231 (3), p.533-547 |
| issn | 0954-4100 2041-3025 |
| language | eng |
| recordid | cdi_proquest_journals_2424920442 |
| source | SAGE Complete |
| subjects | Algorithms Attitude stability Computer simulation Control algorithms Control stability Controllers Equations of motion Euler angles Flexible spacecraft Nonlinear equations Parameter uncertainty Robust control Sliding mode control Spacecraft Spacecraft attitude control Spacecraft stability Spacecraft tracking Stability analysis State observers Tracking control Vibration control |
| title | Robust dynamic surface sliding mode control for attitude tracking of flexible spacecraft with an extended state observer |
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