Comparative analysis of control performances applied to a 3-DOFs nonlinear supersonic lifting surface

Kwan Wook Kim; Bokhee Lee; Sungsoo Na; Pier Marzocca; Attilio Milanese

doi:10.2514/6.2008-1724

Comparative analysis of control performances applied to a 3-DOFs nonlinear supersonic lifting surface

Kwan Wook Kim, Bokhee Lee, Sungsoo Na, Pier Marzocca, Attilio Milanese

Research output: Contribution to journal › Conference article › peer-review

4 Citations (Scopus)

Abstract

This paper presents a comparative analysis of control strategies applied to a nonlinear 2-D wing-flap system operating in supersonic/hypersonic flight speed regimes. Open and closed-loop aeroelastic response and flutter of 2-D supersonic lifting surfaces are investigated. In this context, the implications of aerodynamic and structural nonlinearities on the aeroelastic response in the post-flutter range are presented and various robust control methodologies, such as sliding mode control, H_∞ and fuzzy logic control, are compared. The controls' effectiveness in reducing the aeroelastic vibrations in the various flight speed ranges and in suppressing flutter is demonstrated.

Original language	English
Article number	2008-1724
Journal	Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
DOIs	https://doi.org/10.2514/6.2008-1724
Publication status	Published - 2008
Event	49th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference - Schaumburg, IL, United States Duration: 2008 Apr 7 → 2008 Apr 10

ASJC Scopus subject areas

Architecture
Materials Science(all)
Aerospace Engineering
Mechanics of Materials
Mechanical Engineering

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title = "Comparative analysis of control performances applied to a 3-DOFs nonlinear supersonic lifting surface",

abstract = "This paper presents a comparative analysis of control strategies applied to a nonlinear 2-D wing-flap system operating in supersonic/hypersonic flight speed regimes. Open and closed-loop aeroelastic response and flutter of 2-D supersonic lifting surfaces are investigated. In this context, the implications of aerodynamic and structural nonlinearities on the aeroelastic response in the post-flutter range are presented and various robust control methodologies, such as sliding mode control, H∞ and fuzzy logic control, are compared. The controls' effectiveness in reducing the aeroelastic vibrations in the various flight speed ranges and in suppressing flutter is demonstrated.",

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journal = "Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference",

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T1 - Comparative analysis of control performances applied to a 3-DOFs nonlinear supersonic lifting surface

AU - Kim, Kwan Wook

AU - Lee, Bokhee

AU - Na, Sungsoo

AU - Marzocca, Pier

AU - Milanese, Attilio

PY - 2008

Y1 - 2008

N2 - This paper presents a comparative analysis of control strategies applied to a nonlinear 2-D wing-flap system operating in supersonic/hypersonic flight speed regimes. Open and closed-loop aeroelastic response and flutter of 2-D supersonic lifting surfaces are investigated. In this context, the implications of aerodynamic and structural nonlinearities on the aeroelastic response in the post-flutter range are presented and various robust control methodologies, such as sliding mode control, H∞ and fuzzy logic control, are compared. The controls' effectiveness in reducing the aeroelastic vibrations in the various flight speed ranges and in suppressing flutter is demonstrated.

AB - This paper presents a comparative analysis of control strategies applied to a nonlinear 2-D wing-flap system operating in supersonic/hypersonic flight speed regimes. Open and closed-loop aeroelastic response and flutter of 2-D supersonic lifting surfaces are investigated. In this context, the implications of aerodynamic and structural nonlinearities on the aeroelastic response in the post-flutter range are presented and various robust control methodologies, such as sliding mode control, H∞ and fuzzy logic control, are compared. The controls' effectiveness in reducing the aeroelastic vibrations in the various flight speed ranges and in suppressing flutter is demonstrated.

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M3 - Conference article

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SN - 0273-4508

JO - Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference

JF - Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference

M1 - 2008-1724

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Comparative analysis of control performances applied to a 3-DOFs nonlinear supersonic lifting surface

Abstract

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