Reconfigurable fault-tolerant attitude control for over-actuated hypersonic flight vehicle with actuator failures
This paper proposes a novel fast attitude fault-tolerant control (FTC) scheme for over-actuated hypersonic flight vehicles experiencing actuator failures, such as stuck faults and loss of effectiveness faults. The FTC scheme comprises two main components: a systematic algorithm in the control layer...
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| Vydáno v: | Alexandria engineering journal Ročník 114; s. 463 - 475 |
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| Médium: | Journal Article |
| Jazyk: | angličtina |
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Elsevier B.V
01.02.2025
Elsevier |
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| ISSN: | 1110-0168 |
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| Abstract | This paper proposes a novel fast attitude fault-tolerant control (FTC) scheme for over-actuated hypersonic flight vehicles experiencing actuator failures, such as stuck faults and loss of effectiveness faults. The FTC scheme comprises two main components: a systematic algorithm in the control layer and a control allocation method in the reconfiguration layer, working together to achieve fault tolerance. Drawing inspiration from model predictive static programming, a step-by-step algorithm is developed to quickly resolve control torque under fault conditions, ensuring prescribed tracking performance. The vehicle system's coupling and uncertain disturbances are treated as total disturbance and estimated in real-time using an extended state observer. In the reconfiguration layer, a pseudo-inverse-based control allocation method is utilized to distribute the desired control torque across redundant rudder actuators. The proposed FTC scheme is applied to a hypersonic flight vehicle system subject to stuck faults, loss of effectiveness faults, modeling errors, and external disturbances. Simulation results are presented to demonstrate the superiority and effectiveness of the proposed FTC scheme. Owing to its fast computational speed, the scheme holds potential for online implementation, enabling rapid reconstruction of aerodynamic rudder actuators during failures. |
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| AbstractList | This paper proposes a novel fast attitude fault-tolerant control (FTC) scheme for over-actuated hypersonic flight vehicles experiencing actuator failures, such as stuck faults and loss of effectiveness faults. The FTC scheme comprises two main components: a systematic algorithm in the control layer and a control allocation method in the reconfiguration layer, working together to achieve fault tolerance. Drawing inspiration from model predictive static programming, a step-by-step algorithm is developed to quickly resolve control torque under fault conditions, ensuring prescribed tracking performance. The vehicle system's coupling and uncertain disturbances are treated as total disturbance and estimated in real-time using an extended state observer. In the reconfiguration layer, a pseudo-inverse-based control allocation method is utilized to distribute the desired control torque across redundant rudder actuators. The proposed FTC scheme is applied to a hypersonic flight vehicle system subject to stuck faults, loss of effectiveness faults, modeling errors, and external disturbances. Simulation results are presented to demonstrate the superiority and effectiveness of the proposed FTC scheme. Owing to its fast computational speed, the scheme holds potential for online implementation, enabling rapid reconstruction of aerodynamic rudder actuators during failures. |
| Author | Hu, Xiaoxiang Li, Ao Dong, Kejun Li, Hongzeng Xiao, Bing |
| Author_xml | – sequence: 1 givenname: Ao surname: Li fullname: Li, Ao organization: School of Automation, Northwestern Polytechnical University, Xi’an 710072, PR China – sequence: 2 givenname: Xiaoxiang orcidid: 0000-0001-7047-1949 surname: Hu fullname: Hu, Xiaoxiang email: huxiaoxiang2008@gmail.com organization: School of Automation, Northwestern Polytechnical University, Xi’an 710072, PR China – sequence: 3 givenname: Kejun surname: Dong fullname: Dong, Kejun organization: School of Automation, Northwestern Polytechnical University, Xi’an 710072, PR China – sequence: 4 givenname: Hongzeng surname: Li fullname: Li, Hongzeng organization: 204 Unit, Xi’an Research Institute of High-tech, Xi’an 710025, PR China – sequence: 5 givenname: Bing surname: Xiao fullname: Xiao, Bing organization: School of Automation, Northwestern Polytechnical University, Xi’an 710072, PR China |
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| Keywords | ESO TD MPC LOE FTC MPSP Fault-tolerant control HFV Hypersonic flight vehicles CA Model predictive static programming Control allocation |
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| SubjectTerms | Control allocation Fault-tolerant control Hypersonic flight vehicles Model predictive static programming |
| Title | Reconfigurable fault-tolerant attitude control for over-actuated hypersonic flight vehicle with actuator failures |
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