Neural control of hypersonic flight dynamics with actuator fault and constraint
This paper deals with the control problem of actuator fault and saturation for hypersonic flight vehicles. Different from previous back-stepping design, the scheme is on transforming the dynamics into the "prediction function". The controller is constructed with high gain observer, while the effect...
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| Published in | Science China. Information sciences Vol. 58; no. 7; pp. 68 - 77 |
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| Main Authors | , , , |
| Format | Journal Article |
| Language | English |
| Published |
Beijing
Science China Press
01.07.2015
Springer Nature B.V |
| Subjects | |
| Online Access | Get full text |
| ISSN | 1674-733X 1869-1919 |
| DOI | 10.1007/s11432-015-5338-2 |
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| Summary: | This paper deals with the control problem of actuator fault and saturation for hypersonic flight vehicles. Different from previous back-stepping design, the scheme is on transforming the dynamics into the "prediction function". The controller is constructed with high gain observer, while the effect of fault and saturation is compensated by neural networks. For the input saturation, the auxiliary dynamics is included to design the adaptive learning law. The neural weights and filtered tracking error are guaranteed to be bounded via Lyapunov approach. The effectiveness of the proposed method is verified by simulation of winged-cone model. |
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| Bibliography: | 11-5847/TP This paper deals with the control problem of actuator fault and saturation for hypersonic flight vehicles. Different from previous back-stepping design, the scheme is on transforming the dynamics into the "prediction function". The controller is constructed with high gain observer, while the effect of fault and saturation is compensated by neural networks. For the input saturation, the auxiliary dynamics is included to design the adaptive learning law. The neural weights and filtered tracking error are guaranteed to be bounded via Lyapunov approach. The effectiveness of the proposed method is verified by simulation of winged-cone model. hypersonic flight vehicle, no back-stepping, neural network, longitudinal dynamics, stability ObjectType-Article-1 SourceType-Scholarly Journals-1 ObjectType-Feature-2 content type line 14 |
| ISSN: | 1674-733X 1869-1919 |
| DOI: | 10.1007/s11432-015-5338-2 |