High-order sliding mode attitude controller design for reentry flight
A novel high-order sliding mode control strategy is proposed for the attitude control problem of reentry vehicles in the presence of parametric uncertainties and external disturbances, which results in the robust and accurate tracking of the aerodynamic angle commands with the finite time convergenc...
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| Veröffentlicht in: | Journal of systems engineering and electronics 2014-10, Vol.25 (5), p.848-858 |
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| creator | Wang, Liang Sheng, Yongzhi Liu, Xiangdong |
| description | A novel high-order sliding mode control strategy is proposed for the attitude control problem of reentry vehicles in the presence of parametric uncertainties and external disturbances, which results in the robust and accurate tracking of the aerodynamic angle commands with the finite time convergence. The proposed control strategy is developed on the basis of integral sliding mode philosophy, which combines conventional sliding mode control and a linear quadratic regulator over a finite time interval with a free-final-state and allows the finite-time establishment of a high-order sliding mode. Firstly, a second-order sliding mode attitude controller is designed in the proposed high-order siding mode control framework. Then, to address the control chattering problem, a virtual control is introduced in the control design and hence a third-order sliding mode attitude controller is developed, leading to the chattering reduction as well as the control accuracy improvement. Finally, simulation examples are given to illustrate the effectiveness of the theoretical results. |
| doi_str_mv | 10.1109/JSEE.2014.00098 |
| format | Article |
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The proposed control strategy is developed on the basis of integral sliding mode philosophy, which combines conventional sliding mode control and a linear quadratic regulator over a finite time interval with a free-final-state and allows the finite-time establishment of a high-order sliding mode. Firstly, a second-order sliding mode attitude controller is designed in the proposed high-order siding mode control framework. Then, to address the control chattering problem, a virtual control is introduced in the control design and hence a third-order sliding mode attitude controller is developed, leading to the chattering reduction as well as the control accuracy improvement. Finally, simulation examples are given to illustrate the effectiveness of the theoretical results.</description><identifier>ISSN: 1004-4132</identifier><identifier>EISSN: 1004-4132</identifier><identifier>DOI: 10.1109/JSEE.2014.00098</identifier><language>eng</language><publisher>School of Automation, Beijing Institute of Technology, Beijing 100081, China</publisher><subject>Design engineering ; Mathematical analysis ; Philosophy ; Siding ; Sliding mode ; Sliding mode control ; Strategy ; Vibration ; 再入飞行 ; 参数不确定性 ; 姿态控制器 ; 控制器设计 ; 有限时间收敛 ; 滑动模式控制 ; 线性二次型调节器 ; 高阶滑模</subject><ispartof>Journal of systems engineering and electronics, 2014-10, Vol.25 (5), p.848-858</ispartof><rights>Copyright © Wanfang Data Co. Ltd. All Rights Reserved.</rights><lds50>peer_reviewed</lds50><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c379t-94c87831073566e1c6dce58de2f612fe2d610722d1e25037f4d7a06e774f6b533</citedby></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Uhttp://image.cqvip.com/vip1000/qk/85918X/85918X.jpg</thumbnail><link.rule.ids>315,781,785,27929,27930</link.rule.ids></links><search><creatorcontrib>Wang, Liang</creatorcontrib><creatorcontrib>Sheng, Yongzhi</creatorcontrib><creatorcontrib>Liu, Xiangdong</creatorcontrib><title>High-order sliding mode attitude controller design for reentry flight</title><title>Journal of systems engineering and electronics</title><addtitle>Journal of Systems Engineering and Electronics</addtitle><description>A novel high-order sliding mode control strategy is proposed for the attitude control problem of reentry vehicles in the presence of parametric uncertainties and external disturbances, which results in the robust and accurate tracking of the aerodynamic angle commands with the finite time convergence. The proposed control strategy is developed on the basis of integral sliding mode philosophy, which combines conventional sliding mode control and a linear quadratic regulator over a finite time interval with a free-final-state and allows the finite-time establishment of a high-order sliding mode. Firstly, a second-order sliding mode attitude controller is designed in the proposed high-order siding mode control framework. Then, to address the control chattering problem, a virtual control is introduced in the control design and hence a third-order sliding mode attitude controller is developed, leading to the chattering reduction as well as the control accuracy improvement. Finally, simulation examples are given to illustrate the effectiveness of the theoretical results.</description><subject>Design engineering</subject><subject>Mathematical analysis</subject><subject>Philosophy</subject><subject>Siding</subject><subject>Sliding mode</subject><subject>Sliding mode control</subject><subject>Strategy</subject><subject>Vibration</subject><subject>再入飞行</subject><subject>参数不确定性</subject><subject>姿态控制器</subject><subject>控制器设计</subject><subject>有限时间收敛</subject><subject>滑动模式控制</subject><subject>线性二次型调节器</subject><subject>高阶滑模</subject><issn>1004-4132</issn><issn>1004-4132</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2014</creationdate><recordtype>article</recordtype><recordid>eNpNkDFPwzAQRiMEElXpzBoxMZD27CR2MqKqUFAlBmC2gn1OU6V2ayeC8utxaIXw4pP9vjvdi6JrAlNCoJw9vy4WUwokmwJAWZxFIwKQJRlJ6fm_-jKaeL-B4XCgFEbRYtnU68Q6hS72baMaU8dbqzCuuq7p-lBIazpn2zYACn1Tm1hbFzvE8HyIdRvy3VV0oavW4-R0j6P3h8XbfJmsXh6f5verRKa87JIykwUvUgI8zRlDIpmSmBcKqWaEaqSKhT9KFUGaQ8p1pngFDDnPNPvI03Qc3R37flZGV6YWG9s7EyaKr66WB_W98QIHDZAD4QG_PeI7Z_c9-k5sGy-xbSuDtveCMAaQ85KQgM6OqHTWe4da7FyzrdxBEBCDYjEoFkNv8as4JG5OibU19T6I-4swRnlYNKz5A24eeLg</recordid><startdate>20141001</startdate><enddate>20141001</enddate><creator>Wang, Liang</creator><creator>Sheng, Yongzhi</creator><creator>Liu, Xiangdong</creator><general>School of Automation, Beijing Institute of Technology, Beijing 100081, China</general><general>Key Laboratory for Intelligent Control & Decision of Complex Systems, Beijing Institute of Technology, Beijing 100081, China</general><scope>2RA</scope><scope>92L</scope><scope>CQIGP</scope><scope>~WA</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>7SP</scope><scope>8FD</scope><scope>L7M</scope><scope>2B.</scope><scope>4A8</scope><scope>92I</scope><scope>93N</scope><scope>PSX</scope><scope>TCJ</scope></search><sort><creationdate>20141001</creationdate><title>High-order sliding mode attitude controller design for reentry flight</title><author>Wang, Liang ; Sheng, Yongzhi ; Liu, Xiangdong</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c379t-94c87831073566e1c6dce58de2f612fe2d610722d1e25037f4d7a06e774f6b533</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2014</creationdate><topic>Design engineering</topic><topic>Mathematical analysis</topic><topic>Philosophy</topic><topic>Siding</topic><topic>Sliding mode</topic><topic>Sliding mode control</topic><topic>Strategy</topic><topic>Vibration</topic><topic>再入飞行</topic><topic>参数不确定性</topic><topic>姿态控制器</topic><topic>控制器设计</topic><topic>有限时间收敛</topic><topic>滑动模式控制</topic><topic>线性二次型调节器</topic><topic>高阶滑模</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Wang, Liang</creatorcontrib><creatorcontrib>Sheng, Yongzhi</creatorcontrib><creatorcontrib>Liu, Xiangdong</creatorcontrib><collection>中文科技期刊数据库</collection><collection>中文科技期刊数据库-CALIS站点</collection><collection>中文科技期刊数据库-7.0平台</collection><collection>中文科技期刊数据库- 镜像站点</collection><collection>CrossRef</collection><collection>Electronics & Communications Abstracts</collection><collection>Technology Research Database</collection><collection>Advanced Technologies Database with Aerospace</collection><collection>Wanfang Data Journals - Hong Kong</collection><collection>WANFANG Data Centre</collection><collection>Wanfang Data Journals</collection><collection>万方数据期刊 - 香港版</collection><collection>China Online Journals (COJ)</collection><collection>China Online Journals (COJ)</collection><jtitle>Journal of systems engineering and electronics</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Wang, Liang</au><au>Sheng, Yongzhi</au><au>Liu, Xiangdong</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>High-order sliding mode attitude controller design for reentry flight</atitle><jtitle>Journal of systems engineering and electronics</jtitle><addtitle>Journal of Systems Engineering and Electronics</addtitle><date>2014-10-01</date><risdate>2014</risdate><volume>25</volume><issue>5</issue><spage>848</spage><epage>858</epage><pages>848-858</pages><issn>1004-4132</issn><eissn>1004-4132</eissn><abstract>A novel high-order sliding mode control strategy is proposed for the attitude control problem of reentry vehicles in the presence of parametric uncertainties and external disturbances, which results in the robust and accurate tracking of the aerodynamic angle commands with the finite time convergence. 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| identifier | ISSN: 1004-4132 |
| ispartof | Journal of systems engineering and electronics, 2014-10, Vol.25 (5), p.848-858 |
| issn | 1004-4132 1004-4132 |
| language | eng |
| recordid | cdi_wanfang_journals_xtgcydzjs_e201405017 |
| source | IEEE Power & Energy Library; EZB-FREE-00999 freely available EZB journals |
| subjects | Design engineering Mathematical analysis Philosophy Siding Sliding mode Sliding mode control Strategy Vibration 再入飞行 参数不确定性 姿态控制器 控制器设计 有限时间收敛 滑动模式控制 线性二次型调节器 高阶滑模 |
| title | High-order sliding mode attitude controller design for reentry flight |
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