Abstract
Robust fault-tolerant control problem is investigated for Hyper-X hypersonic vehicle attitude control system. Based on parameter-dependent Lyapunov functions, robust fault-tolerant H static feedback controller is designed for actuator faults. The sufficient conditions, guaranteeing that the hypersonic vehicle is robust fault-tolerant stable with H index constraints, are obtained for the design of static feedback controller in terms of linear matrix inequalities (LMIs). Finally, an application to numerical example shows the effectiveness of the proposed methods.
| Original language | English |
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| Title of host publication | Proceedings of the 30th Chinese Control Conference, CCC 2011 |
| Pages | 4313-4316 |
| Number of pages | 4 |
| Publication status | Published - 2011 |
| Event | 30th Chinese Control Conference, CCC 2011 - Yantai, China Duration: 22 Jul 2011 → 24 Jul 2011 |
Publication series
| Name | Proceedings of the 30th Chinese Control Conference, CCC 2011 |
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Conference
| Conference | 30th Chinese Control Conference, CCC 2011 |
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| Country/Territory | China |
| City | Yantai |
| Period | 22/07/11 → 24/07/11 |
Keywords
- H control
- Hypersonic vehicle
- Linear matrix inequality (LMI)
- Parameter-dependent Lyapunov functions
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Lu, P., & Liu, X. (2011). Robust fault-tolerant H∞ control for hypersonic vehicle attitude control system. In Proceedings of the 30th Chinese Control Conference, CCC 2011 (pp. 4313-4316). Article 6001337 (Proceedings of the 30th Chinese Control Conference, CCC 2011).