Finite-Time Control for Attitude Tracking Maneuver of Rigid Satellite
The problem of finite-time control for attitude tracking maneuver of a rigid spacecraft is investigated. External disturbance, unknown inertia parameters are addressed. As stepping stone, a sliding mode controller is designed. It requires the upper bound of the lumped uncertainty including disturban...
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| Format: | Article |
| Language: | English |
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Wiley
2014-01-01
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| Series: | Abstract and Applied Analysis |
| Online Access: | http://dx.doi.org/10.1155/2014/302982 |
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| _version_ | 1832550731689754624 |
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| author | Mingyi Huo Xing Huo Hamid Reza Karimi Jianfei Ni |
| author_facet | Mingyi Huo Xing Huo Hamid Reza Karimi Jianfei Ni |
| author_sort | Mingyi Huo |
| collection | DOAJ |
| description | The problem of finite-time control for attitude tracking maneuver of a rigid spacecraft is investigated. External disturbance, unknown inertia parameters are addressed. As stepping stone, a sliding mode controller is designed. It requires the upper bound of the lumped uncertainty including disturbance and inertia matrix. However, this upper bound may not be easily obtained. Therefore, an adaptive sliding mode control law is then proposed to release that drawback. Adaptive technique is applied to estimate that bound. It is proved that the closed-loop attitude tracking system is finite-time stable. The tracking errors of the attitude and the angular velocity are asymptotically stabilized. Moreover, the upper bound on the lumped uncertainty can be exactly estimated in finite time. The attitude tracking performance with application of the control scheme is evaluated through a numerical example. |
| format | Article |
| id | doaj-art-db8164217b6a43d5a9bb3088d652104a |
| institution | Kabale University |
| issn | 1085-3375 1687-0409 |
| language | English |
| publishDate | 2014-01-01 |
| publisher | Wiley |
| record_format | Article |
| series | Abstract and Applied Analysis |
| spelling | doaj-art-db8164217b6a43d5a9bb3088d652104a2025-02-03T06:06:08ZengWileyAbstract and Applied Analysis1085-33751687-04092014-01-01201410.1155/2014/302982302982Finite-Time Control for Attitude Tracking Maneuver of Rigid SatelliteMingyi Huo0Xing Huo1Hamid Reza Karimi2Jianfei Ni3Department of Control Science and Engineering, Harbin Institute of Technology, Harbin 150001, ChinaCollege of Engineering, Bohai University, Jinzhou 121000, ChinaDepartment of Engineering, Faculty of Engineering and Science, The University of Agder, 4898 Grimstad, NorwayCollege of Engineering, Bohai University, Jinzhou 121000, ChinaThe problem of finite-time control for attitude tracking maneuver of a rigid spacecraft is investigated. External disturbance, unknown inertia parameters are addressed. As stepping stone, a sliding mode controller is designed. It requires the upper bound of the lumped uncertainty including disturbance and inertia matrix. However, this upper bound may not be easily obtained. Therefore, an adaptive sliding mode control law is then proposed to release that drawback. Adaptive technique is applied to estimate that bound. It is proved that the closed-loop attitude tracking system is finite-time stable. The tracking errors of the attitude and the angular velocity are asymptotically stabilized. Moreover, the upper bound on the lumped uncertainty can be exactly estimated in finite time. The attitude tracking performance with application of the control scheme is evaluated through a numerical example.http://dx.doi.org/10.1155/2014/302982 |
| spellingShingle | Mingyi Huo Xing Huo Hamid Reza Karimi Jianfei Ni Finite-Time Control for Attitude Tracking Maneuver of Rigid Satellite Abstract and Applied Analysis |
| title | Finite-Time Control for Attitude Tracking Maneuver of Rigid Satellite |
| title_full | Finite-Time Control for Attitude Tracking Maneuver of Rigid Satellite |
| title_fullStr | Finite-Time Control for Attitude Tracking Maneuver of Rigid Satellite |
| title_full_unstemmed | Finite-Time Control for Attitude Tracking Maneuver of Rigid Satellite |
| title_short | Finite-Time Control for Attitude Tracking Maneuver of Rigid Satellite |
| title_sort | finite time control for attitude tracking maneuver of rigid satellite |
| url | http://dx.doi.org/10.1155/2014/302982 |
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