Sliding mode robust control of supersonic three degrees-of-freedom airfoils

Bok Hee Lee; Jeong Hwan Choo; Sungsoo Na; Piergiovanni Marzocca; Liviu Librescu

doi:10.1007/s12555-010-0214-8

Sliding mode robust control of supersonic three degrees-of-freedom airfoils

Bok Hee Lee, Jeong Hwan Choo, Sungsoo Na, Piergiovanni Marzocca, Liviu Librescu

Research output: Contribution to journal › Article › peer-review

11 Citations (Scopus)

Abstract

The robust aeroelastic control of a three-degrees-of-freedom (3DOF) linear and non-linear wing-flap system under sliding mode control (SMC) and operation in supersonic flight speeds is presented. Open- and closed-loop aeroelastic responses to blast and sonic-boom excitation in the wingflap system with uncertainty, as well as flutter analysis, are investigated along with the implementation of a Sliding Mode Observer (SMO). The effectiveness of control in reducing the amplitude of oscillation and preventing flutter instability is demonstrated.

Original language	English
Pages (from-to)	279-288
Number of pages	10
Journal	International Journal of Control, Automation and Systems
Volume	8
Issue number	2
DOIs	https://doi.org/10.1007/s12555-010-0214-8
Publication status	Published - 2010 Apr

Keywords

3DOF airfoil system
Aeroelasticity
Sliding mode control
Sliding mode observer

ASJC Scopus subject areas

Control and Systems Engineering
Computer Science Applications

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10.1007/s12555-010-0214-8

Cite this

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title = "Sliding mode robust control of supersonic three degrees-of-freedom airfoils",

abstract = "The robust aeroelastic control of a three-degrees-of-freedom (3DOF) linear and non-linear wing-flap system under sliding mode control (SMC) and operation in supersonic flight speeds is presented. Open- and closed-loop aeroelastic responses to blast and sonic-boom excitation in the wingflap system with uncertainty, as well as flutter analysis, are investigated along with the implementation of a Sliding Mode Observer (SMO). The effectiveness of control in reducing the amplitude of oscillation and preventing flutter instability is demonstrated.",

keywords = "3DOF airfoil system, Aeroelasticity, Sliding mode control, Sliding mode observer",

author = "Lee, {Bok Hee} and Choo, {Jeong Hwan} and Sungsoo Na and Piergiovanni Marzocca and Liviu Librescu",

note = "Funding Information: Manuscript received December 11, 2008; revised July 25, 2009; accepted October 23, 2009. Recommended by Editorial Board member Hyo-Choong Bang under the direction of Editor Jae Weon Choi. The authors would like to acknowledge the late Professor Liviu Librescu of Virginia Tech, who help, guide and support through the years have made this research possible. He will be remembered and deeply missed. S. Na also acknowledges the financial support from KOSEF (No. 2009-0063170).",

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doi = "10.1007/s12555-010-0214-8",

language = "English",

volume = "8",

pages = "279--288",

journal = "International Journal of Control, Automation and Systems",

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T1 - Sliding mode robust control of supersonic three degrees-of-freedom airfoils

AU - Lee, Bok Hee

AU - Choo, Jeong Hwan

AU - Na, Sungsoo

AU - Marzocca, Piergiovanni

AU - Librescu, Liviu

N1 - Funding Information: Manuscript received December 11, 2008; revised July 25, 2009; accepted October 23, 2009. Recommended by Editorial Board member Hyo-Choong Bang under the direction of Editor Jae Weon Choi. The authors would like to acknowledge the late Professor Liviu Librescu of Virginia Tech, who help, guide and support through the years have made this research possible. He will be remembered and deeply missed. S. Na also acknowledges the financial support from KOSEF (No. 2009-0063170).

PY - 2010/4

Y1 - 2010/4

N2 - The robust aeroelastic control of a three-degrees-of-freedom (3DOF) linear and non-linear wing-flap system under sliding mode control (SMC) and operation in supersonic flight speeds is presented. Open- and closed-loop aeroelastic responses to blast and sonic-boom excitation in the wingflap system with uncertainty, as well as flutter analysis, are investigated along with the implementation of a Sliding Mode Observer (SMO). The effectiveness of control in reducing the amplitude of oscillation and preventing flutter instability is demonstrated.

AB - The robust aeroelastic control of a three-degrees-of-freedom (3DOF) linear and non-linear wing-flap system under sliding mode control (SMC) and operation in supersonic flight speeds is presented. Open- and closed-loop aeroelastic responses to blast and sonic-boom excitation in the wingflap system with uncertainty, as well as flutter analysis, are investigated along with the implementation of a Sliding Mode Observer (SMO). The effectiveness of control in reducing the amplitude of oscillation and preventing flutter instability is demonstrated.

KW - 3DOF airfoil system

KW - Aeroelasticity

KW - Sliding mode control

KW - Sliding mode observer

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SP - 279

EP - 288

JO - International Journal of Control, Automation and Systems

JF - International Journal of Control, Automation and Systems

IS - 2

ER -

Sliding mode robust control of supersonic three degrees-of-freedom airfoils

Abstract

Keywords

ASJC Scopus subject areas

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