Event‐Triggered Anti‐Disturbance Attitude Control for Flexible Spacecraft With Unknown Harmonic Disturbances via Adaptive Disturbance Observer
This article addresses the attitude control issue subject to unknown harmonic disturbances and inertial uncertainties for flexible spacecraft based on a dynamic event‐triggered mechanism and a T–S fuzzy modeling method. To estimate the flexible modes, a flexible vibration observer is constructed. An...
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| Published in | International journal of adaptive control and signal processing |
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| Main Authors | , , , |
| Format | Journal Article |
| Language | English |
| Published |
04.03.2025
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| Online Access | Get full text |
| ISSN | 0890-6327 1099-1115 |
| DOI | 10.1002/acs.3969 |
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| Abstract | This article addresses the attitude control issue subject to unknown harmonic disturbances and inertial uncertainties for flexible spacecraft based on a dynamic event‐triggered mechanism and a T–S fuzzy modeling method. To estimate the flexible modes, a flexible vibration observer is constructed. An auxiliary filter is applied to transform unknown harmonic disturbances into an expression with unknown parameters. Then according to the estimations of unknown parameters, an adaptive disturbance observer is constructed. Additionally, the control scheme based on the dynamic event‐triggered mechanism is designed to guarantee the boundedness of all closed‐loop. Finally, two simulation cases are given for disturbances with single frequency and multiple frequencies to show the feasibility and effectiveness of the proposed control strategy. |
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| AbstractList | This article addresses the attitude control issue subject to unknown harmonic disturbances and inertial uncertainties for flexible spacecraft based on a dynamic event‐triggered mechanism and a T–S fuzzy modeling method. To estimate the flexible modes, a flexible vibration observer is constructed. An auxiliary filter is applied to transform unknown harmonic disturbances into an expression with unknown parameters. Then according to the estimations of unknown parameters, an adaptive disturbance observer is constructed. Additionally, the control scheme based on the dynamic event‐triggered mechanism is designed to guarantee the boundedness of all closed‐loop. Finally, two simulation cases are given for disturbances with single frequency and multiple frequencies to show the feasibility and effectiveness of the proposed control strategy. |
| Author | Zhu, Chunjie Sun, Haibin Jiao, Ticao Hou, Linlin |
| Author_xml | – sequence: 1 givenname: Chunjie surname: Zhu fullname: Zhu, Chunjie organization: School of Engineering Qufu Normal University Rizhao China – sequence: 2 givenname: Haibin orcidid: 0000-0002-4447-1758 surname: Sun fullname: Sun, Haibin organization: School of Engineering Qufu Normal University Rizhao China – sequence: 3 givenname: Linlin orcidid: 0000-0001-7321-9239 surname: Hou fullname: Hou, Linlin organization: School of Computer Qufu Normal University Rizhao China – sequence: 4 givenname: Ticao orcidid: 0000-0001-9323-4321 surname: Jiao fullname: Jiao, Ticao organization: School of Electrical and Electronic Engineering Shandong University of Technology Zibo China |
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