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    Sliding Mode Robust Control of Supersonic Three Degrees-of-Freedom Airfoils

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    https://www.riss.kr/link?id=A104905028

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    다국어 초록 (Multilingual Abstract) kakao i 다국어 번역

    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 wing-flap 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.
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    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 an...

    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 wing-flap 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.

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    참고문헌 (Reference)

    1 M. Allen, "Sliding mode control of a large flexible space structure" 8 : 861-871, 2000

    2 C. Edwards, "Sliding Mode Control - Theory and Applications" Taylor and Francis 1998

    3 S. Na, "Robust aeroelastic control of two-dimensional supersonic flapped wing systems" 192 (192): 37-47, 2007

    4 S. Na, "Robust aeroelastic control of 2-d supersonic flapped lifting surfaces" 2006

    5 H. Ashley, "Piston theory - a new aerodynamic tool for the aeroelastician" 23 (23): 1109-1118, 1956

    6 P. Marzocca, "Nonlinear aeroelastic response and control of supersonic flapped 2-D lifting surfaces" 2006

    7 M. Kim, "Nonlinear Control and Robust Observer Design for Marine Vehicles" VPI&SU 2000

    8 R. H. Scanlan, "Introduction to the Study of Aircraft Vibration and Flutter" The Macmillan Co. 1951

    9 V.Mukhopadhyay, "Flutter suppression control law design and testing for the active flexible wing" 32 : 45-51, 1995

    10 M.J.Balas, "Feedback control of flexible systems" 23 (23): 673-679, 1978

    1 M. Allen, "Sliding mode control of a large flexible space structure" 8 : 861-871, 2000

    2 C. Edwards, "Sliding Mode Control - Theory and Applications" Taylor and Francis 1998

    3 S. Na, "Robust aeroelastic control of two-dimensional supersonic flapped wing systems" 192 (192): 37-47, 2007

    4 S. Na, "Robust aeroelastic control of 2-d supersonic flapped lifting surfaces" 2006

    5 H. Ashley, "Piston theory - a new aerodynamic tool for the aeroelastician" 23 (23): 1109-1118, 1956

    6 P. Marzocca, "Nonlinear aeroelastic response and control of supersonic flapped 2-D lifting surfaces" 2006

    7 M. Kim, "Nonlinear Control and Robust Observer Design for Marine Vehicles" VPI&SU 2000

    8 R. H. Scanlan, "Introduction to the Study of Aircraft Vibration and Flutter" The Macmillan Co. 1951

    9 V.Mukhopadhyay, "Flutter suppression control law design and testing for the active flexible wing" 32 : 45-51, 1995

    10 M.J.Balas, "Feedback control of flexible systems" 23 (23): 673-679, 1978

    11 G. C. Goodwin, "Control System Design" Prentice-Hall, Inc. 2001

    12 V. Mukhopadhyay, "Benchmark active controlv technology" 23 : 913-1139, 2000

    13 P. Marzocca, "Aeroelastic response of 2-d lifting surface to gust and arbitrary explosive loading signatures" 25 : 41-65, 2001

    14 L. Librescu, "Advances in the linear/non-linear control of aeroelastic structural systems" 178 (178): 147-186, 2005

    15 D.J.Inman, "Active modal control for smart structures in Philosophical Transactions: Mathematical" Physical & Engineering Sciences 205-219, 2000

    16 L. Librescu, "Active aeroelastic control of 2-d wing-flap systems operating in an incompressible flowfield and impacted by a blast pulse" 283 (283): 685-706, 2005

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    연월일 이력구분 이력상세 등재구분
    2023 평가 해외DB학술지평가 신청대상 (해외등재 학술지 평가)
    2020-01-01 등재 등재학술지 유지 (해외등재 학술지 평가) KCI등재
    2010-01-01 등재 등재학술지 유지 (등재유지) KCI등재
    2009-12-29 학회명변경 한글명 : 제어ㆍ로봇ㆍ시스템학회 -> 제어·로봇·시스템학회 KCI등재
    2008-01-01 등재 등재학술지 유지 (등재유지) KCI등재
    2007-10-29 학회명변경 한글명 : 제어ㆍ자동화ㆍ시스템공학회 -> 제어ㆍ로봇ㆍ시스템학회
    영문명 : The Institute Of Control, Automation, And Systems Engineers, Korea -> Institute of Control, Robotics and Systems
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    2005-01-01 등재 등재학술지 선정 (등재후보2차) KCI등재
    2004-01-01 등재 등재후보 1차 PASS (등재후보1차) KCI등재후보
    2002-07-01 등재 등재후보학술지 선정 (신규평가) KCI등재후보
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    기준연도 WOS-KCI 통합IF(2년) KCIF(2년) KCIF(3년)
    2016 1.35 0.6 1.07
    KCIF(4년) KCIF(5년) 중심성지수(3년) 즉시성지수
    0.88 0.73 0.388 0.04
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