Prescribed Performance Tracking Control for the Hypersonic Vehicle with Actuator Faults
This paper provides a solution for the trajectory tracking control of a hypersonic flight vehicle (HFV), which is encountered performance constraints, actuator faults, external disturbances, and system uncertainties. For the altitude and velocity control subsystems, the backstepping-based dynamic su...
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| Main Authors: | , , , , , |
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| Format: | Article |
| Language: | English |
| Published: |
Wiley
2021-01-01
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| Series: | International Journal of Aerospace Engineering |
| Online Access: | http://dx.doi.org/10.1155/2021/8880387 |
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| _version_ | 1832563268259938304 |
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| author | Zhenghui Yang Wentao He Yushan He Yaen Xie Jun Li Shuo Song |
| author_facet | Zhenghui Yang Wentao He Yushan He Yaen Xie Jun Li Shuo Song |
| author_sort | Zhenghui Yang |
| collection | DOAJ |
| description | This paper provides a solution for the trajectory tracking control of a hypersonic flight vehicle (HFV), which is encountered performance constraints, actuator faults, external disturbances, and system uncertainties. For the altitude and velocity control subsystems, the backstepping-based dynamic surface control (DSC) strategy is constructed to guarantee the predefined constraint of tracking errors. The introduction of first-order low-pass filters effectively remedies the problem of “complexity explosion” existing in high-order backstepping design. Simultaneously, radial basis function neural networks (RBFNNs) are adopted for approximating the unavailable dynamics, in which the minimum learning parameter (MLP) algorithm brilliantly alleviates the excessive occupation of the computational resource. Specially, in consideration of the unknown actuator failures, the adaptive signals are designed to enhance the reliability of the closed-loop system. Finally, according to rigorous theoretical analysis and simulation experiment, the stability of the proposed controller is verified, and its superiority is exhibited intuitively. |
| format | Article |
| id | doaj-art-10519aea47084c2e8dae549c7d53af53 |
| institution | Kabale University |
| issn | 1687-5966 1687-5974 |
| language | English |
| publishDate | 2021-01-01 |
| publisher | Wiley |
| record_format | Article |
| series | International Journal of Aerospace Engineering |
| spelling | doaj-art-10519aea47084c2e8dae549c7d53af532025-02-03T01:20:32ZengWileyInternational Journal of Aerospace Engineering1687-59661687-59742021-01-01202110.1155/2021/88803878880387Prescribed Performance Tracking Control for the Hypersonic Vehicle with Actuator FaultsZhenghui Yang0Wentao He1Yushan He2Yaen Xie3Jun Li4Shuo Song5School of Geological Engineering and Geomatics, Chang’an University, ChinaCollege of Aerospace and Civil Engineering, Harbin Engineering University, ChinaSchool of Automation, Harbin Engineering University, ChinaCollege of Aerospace and Civil Engineering, Harbin Engineering University, ChinaSchool of Automation, Harbin Engineering University, ChinaSchool of Automation, Harbin Engineering University, ChinaThis paper provides a solution for the trajectory tracking control of a hypersonic flight vehicle (HFV), which is encountered performance constraints, actuator faults, external disturbances, and system uncertainties. For the altitude and velocity control subsystems, the backstepping-based dynamic surface control (DSC) strategy is constructed to guarantee the predefined constraint of tracking errors. The introduction of first-order low-pass filters effectively remedies the problem of “complexity explosion” existing in high-order backstepping design. Simultaneously, radial basis function neural networks (RBFNNs) are adopted for approximating the unavailable dynamics, in which the minimum learning parameter (MLP) algorithm brilliantly alleviates the excessive occupation of the computational resource. Specially, in consideration of the unknown actuator failures, the adaptive signals are designed to enhance the reliability of the closed-loop system. Finally, according to rigorous theoretical analysis and simulation experiment, the stability of the proposed controller is verified, and its superiority is exhibited intuitively.http://dx.doi.org/10.1155/2021/8880387 |
| spellingShingle | Zhenghui Yang Wentao He Yushan He Yaen Xie Jun Li Shuo Song Prescribed Performance Tracking Control for the Hypersonic Vehicle with Actuator Faults International Journal of Aerospace Engineering |
| title | Prescribed Performance Tracking Control for the Hypersonic Vehicle with Actuator Faults |
| title_full | Prescribed Performance Tracking Control for the Hypersonic Vehicle with Actuator Faults |
| title_fullStr | Prescribed Performance Tracking Control for the Hypersonic Vehicle with Actuator Faults |
| title_full_unstemmed | Prescribed Performance Tracking Control for the Hypersonic Vehicle with Actuator Faults |
| title_short | Prescribed Performance Tracking Control for the Hypersonic Vehicle with Actuator Faults |
| title_sort | prescribed performance tracking control for the hypersonic vehicle with actuator faults |
| url | http://dx.doi.org/10.1155/2021/8880387 |
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