Predefined Time Anti-Unwinding Control of Rigid Spacecraft Attitude Tracking
This paper addresses the predefined time anti-unwinding attitude tracking control of rigid spacecraft with inertial uncertainties and external disturbances. Firstly, a new predefined-time terminal sliding surface (FTS) is proposed with hybrid technique. Secondly, a simple predefined-time sliding mod...
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| Main Authors: | , , , , , |
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| Format: | Article |
| Language: | English |
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IEEE
2025-01-01
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| Series: | IEEE Access |
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| Online Access: | https://ieeexplore.ieee.org/document/10839419/ |
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| _version_ | 1832576744290254848 |
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| author | Liangmou Hu Zeng Wang Hanghang Wang Changrui Chen Heng Yue Jiale Wang |
| author_facet | Liangmou Hu Zeng Wang Hanghang Wang Changrui Chen Heng Yue Jiale Wang |
| author_sort | Liangmou Hu |
| collection | DOAJ |
| description | This paper addresses the predefined time anti-unwinding attitude tracking control of rigid spacecraft with inertial uncertainties and external disturbances. Firstly, a new predefined-time terminal sliding surface (FTS) is proposed with hybrid technique. Secondly, a simple predefined-time sliding mode control (PTAC) is exploited to solve the robust attitude tracking problem. It is proved that the proposed PTAC can ensure that the attitude tracking errors tend to an arbitrary small bound centered on equilibrium point within predefined time and then go to equilibrium point asymptotically. The features of the PTAC includes robust, anti-unwinding and predefined time. To verify the effectiveness of the developed scheme, the numerical simulations are demonstrated. |
| format | Article |
| id | doaj-art-30318fbb0f2b42ca93a68fd8fd265dc3 |
| institution | Kabale University |
| issn | 2169-3536 |
| language | English |
| publishDate | 2025-01-01 |
| publisher | IEEE |
| record_format | Article |
| series | IEEE Access |
| spelling | doaj-art-30318fbb0f2b42ca93a68fd8fd265dc32025-01-31T00:01:47ZengIEEEIEEE Access2169-35362025-01-0113190161902510.1109/ACCESS.2025.352903510839419Predefined Time Anti-Unwinding Control of Rigid Spacecraft Attitude TrackingLiangmou Hu0https://orcid.org/0000-0002-4630-6350Zeng Wang1https://orcid.org/0000-0002-3533-9368Hanghang Wang2Changrui Chen3https://orcid.org/0009-0008-4113-2129Heng Yue4https://orcid.org/0009-0006-6415-2961Jiale Wang5Xi’an Key Laboratory of Intelligence, Xi’an Technological University, Xi’an, ChinaXi’an Key Laboratory of Intelligence, Xi’an Technological University, Xi’an, ChinaXi’an Key Laboratory of Intelligence, Xi’an Technological University, Xi’an, ChinaXi’an Key Laboratory of Intelligence, Xi’an Technological University, Xi’an, ChinaXi’an Key Laboratory of Intelligence, Xi’an Technological University, Xi’an, ChinaXi’an Key Laboratory of Intelligence, Xi’an Technological University, Xi’an, ChinaThis paper addresses the predefined time anti-unwinding attitude tracking control of rigid spacecraft with inertial uncertainties and external disturbances. Firstly, a new predefined-time terminal sliding surface (FTS) is proposed with hybrid technique. Secondly, a simple predefined-time sliding mode control (PTAC) is exploited to solve the robust attitude tracking problem. It is proved that the proposed PTAC can ensure that the attitude tracking errors tend to an arbitrary small bound centered on equilibrium point within predefined time and then go to equilibrium point asymptotically. The features of the PTAC includes robust, anti-unwinding and predefined time. To verify the effectiveness of the developed scheme, the numerical simulations are demonstrated.https://ieeexplore.ieee.org/document/10839419/Attitude tracking controlpredefined-timeunwinding problemuncertain spacecraftrobustness |
| spellingShingle | Liangmou Hu Zeng Wang Hanghang Wang Changrui Chen Heng Yue Jiale Wang Predefined Time Anti-Unwinding Control of Rigid Spacecraft Attitude Tracking IEEE Access Attitude tracking control predefined-time unwinding problem uncertain spacecraft robustness |
| title | Predefined Time Anti-Unwinding Control of Rigid Spacecraft Attitude Tracking |
| title_full | Predefined Time Anti-Unwinding Control of Rigid Spacecraft Attitude Tracking |
| title_fullStr | Predefined Time Anti-Unwinding Control of Rigid Spacecraft Attitude Tracking |
| title_full_unstemmed | Predefined Time Anti-Unwinding Control of Rigid Spacecraft Attitude Tracking |
| title_short | Predefined Time Anti-Unwinding Control of Rigid Spacecraft Attitude Tracking |
| title_sort | predefined time anti unwinding control of rigid spacecraft attitude tracking |
| topic | Attitude tracking control predefined-time unwinding problem uncertain spacecraft robustness |
| url | https://ieeexplore.ieee.org/document/10839419/ |
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