Robust fault-tolerant H∞ control for hypersonic vehicle attitude control system

Pingli Lu; Xiangdong Liu

Robust fault-tolerant H_∞ control for hypersonic vehicle attitude control system

Pingli Lu^*, Xiangdong Liu

^*Corresponding author for this work

School of Automation

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

5 Citations (Scopus)

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
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

Conference

Conference	30th Chinese Control Conference, CCC 2011
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

Cite this

@inproceedings{fec2216a88b04dc59925c410c1c843ae,

title = "Robust fault-tolerant H∞ control for hypersonic vehicle attitude control system",

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.",

keywords = "H control, Hypersonic vehicle, Linear matrix inequality (LMI), Parameter-dependent Lyapunov functions",

author = "Pingli Lu and Xiangdong Liu",

year = "2011",

language = "English",

isbn = "9789881725592",

series = "Proceedings of the 30th Chinese Control Conference, CCC 2011",

pages = "4313--4316",

booktitle = "Proceedings of the 30th Chinese Control Conference, CCC 2011",

note = "30th Chinese Control Conference, CCC 2011 ; Conference date: 22-07-2011 Through 24-07-2011",

}

Robust fault-tolerant H_∞ control for hypersonic vehicle attitude control system. / Lu, Pingli ; Liu, Xiangdong.
Proceedings of the 30th Chinese Control Conference, CCC 2011. 2011. p. 4313-4316 6001337 (Proceedings of the 30th Chinese Control Conference, CCC 2011).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

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AU - Liu, Xiangdong

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N2 - 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.

AB - 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.

KW - H control

KW - Hypersonic vehicle

KW - Linear matrix inequality (LMI)

KW - Parameter-dependent Lyapunov functions

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T3 - Proceedings of the 30th Chinese Control Conference, CCC 2011

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BT - Proceedings of the 30th Chinese Control Conference, CCC 2011

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