Finite time Control Scheme for Aeroelastic Systems
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- 英文论文题名：Finite time Control Scheme for Aeroelastic Systems
- 论文作者：Hongqi Zhu ; Miao Chen ; Wei Du ; Honghong Chen
- 英文论文作者：Hongqi Zhu ; Miao Chen ; Wei Du ; Honghong Chen ; Department of Applied Mathematics ; Huainan Normal University
- 年：2017
- 作者机构：Department of Applied Mathematics,Huainan Normal University;
- 英文论文关键词：Alaeroelastic system ; finite time ; sliding mode control ; stability
- 会议召开时间：2017-07-26
- 会议录名称：第36届中国控制会议论文集（A）
- 英文会议录名称：Proceedings of the 36th Chinese Control Conference（A）
- 语种：英文
- 分类号：O231
- 学会代码：KZLL
- 会议名称：第36届中国控制会议
- 会议地点：中国辽宁大连
- 主办单位：中国自动化学会控制理论专业委员会
- 学会名称：中国自动化学会控制理论专业委员会
- 页数：5
- 文件大小：719k
- 原文格式：D
- 会议级别：全国
摘要
This paper is concerned with a finite time control law design to suppress flutter in an alaeroelastic system. Firstly, we design a terminal sliding surface for the alaeroelastic system. Based on Lyapunov stability theory, the stability of the closed-loop system is established. The corresponding numerical simulations are demonstrated to verify the effectiveness of proposed method.
This paper is concerned with a finite time control law design to suppress flutter in an alaeroelastic system. Firstly, we design a terminal sliding surface for the alaeroelastic system. Based on Lyapunov stability theory, the stability of the closed-loop system is established. The corresponding numerical simulations are demonstrated to verify the effectiveness of proposed method.
This paper is concerned with a finite time control law design to suppress flutter in an alaeroelastic system. Firstly, we design a terminal sliding surface for the alaeroelastic system. Based on Lyapunov stability theory, the stability of the closed-loop system is established. The corresponding numerical simulations are demonstrated to verify the effectiveness of proposed method.
引文
[1]G.J.Li,H.Liu,Stability analysis and synchronization for a class of fractional-order neural networks,Entropy,vol.18,no.2,p.55,2016.
[2]R.Rakkiyappan,G.Velmurugan,and J.D.Cao,Stability analysis of fractional-order complex-valued neural networks with time delays,Chaos,Solitons&Fractals,vol.78,pp.297–316,2015.
[3]S.Pei,J.Shyu,Y.Huang,and C.Chan,Improved methods for the design of variable fractional-delay IIR digital filters,IEEE Trans.Circuits Syst.I,Reg.Papers,vol.59,no.5,pp.989-1000,2012.
[4]M.O.Efe,Fractional fuzzy adaptive sliding-mode control of a 2-DOF direct-drive robot arm,IEEE Transactions on Systems,Man,and Cybernetics,vol.38,no.6,pp.1561-1570,2008.
[5]A.H.Nayfeh,D.T.Mook,Nonlinear oscillations,Wiley Inter Science,New York,1995.
[6]E.H.Dowell,Non-linear oscillator models in bluff body aeroelasticity,Journal of Sound and Vibration,vol.75,pp.251-264,1981.
[7]B.vander Pol,J.vander Mark,Frequency demultiplication,Nature,vol.120,pp.363-364,1927.
[8]E.Domany,O.V.Gendelman,Dynamic responses and mitigation of limit cycle oscillations in Van der Pol-Duffing oscillator with nonlinear energy sink,Journal of Sound and Vibration,vol.21,pp.5489-5507,2013.
[9]Y.S.Lee,A.FVakakis,L.A.Bergman,D.M.Mc Farland,Suppression of limit cycle oscillations in the Van der Pol oscillator by means of passive nonlinear energy sinks(NESs),Structural Control and Health Monitoring,vol.13,pp.41-75,2006.
[10]O.V.Gendelman,T.Bar,Bifurcations of self-excitation regimes in a Van der Pol oscillator with a nonlinear energy sink,Physica D,vol.239,pp.220-229,2010.
[11]J.A.Dunnmon,S.C.Stanton,B.P.Mann,et al.,Power extraction from aeroelastic limit cycle oscillations,Journal of Fluids and Structures,vol.27,pp.1182-1198,2011.
[12]A.Drachinsky,D.E.Raveh,Limit-cycle oscillations of a pretensed membrane strip,Journal of Fluids and Structures,vol.60,pp.1-22,2016.
[13]M.Dardel,F.Bakhtiari-Nejad,A reduced order of complete aeroelastic model for limit cycle oscillations,Aerospace science and technology,vol.14,pp.95-105,2010.
[14]S.A.Eftekhari,F.Bakhtiari-Nejad,E.H.Dowell,Damage detection of an aeroelastic panel using limit cycle oscillation analysis,International Journal of Non-Linear Mechanics,vol.58,pp.99-110,2014.
[15]N.G.Bhoir,S.N.Singh,Output feedback nonlinear control of an aeroelastic with unsteady aerodynamics,Aerosp.Sci.Technol.,vol.8,pp.195-205,2004.
[16]T.W.Strganac,D.E.Thompson,Identification and control of limit cycle oscillations in aeroelastic systems,J.Guid.Control Dyn.,vol.23,pp.1127-1133,2008.
[17]S.Gujjula,S.N.Singh,W.Yim,Adaptive and neural control of a wing section using leading-and trailing-edge surfaces,Aerosp.Sci.Technol.,vol.9,pp.161-171,2005.
[18]C.L Chen,C.W.Chang,H.T.Yau,Terminal sliding mode control for aeroelastic systems,Nonlinear Dyn.,vol.70,pp.2015-2026,2013.
[19]C.L.Chen,C.C.Peng,H.T.Yau,High-order sliding mode controller with backstepping design for aeroelastic systems,Commun.Nonlinear Sci.Numer.Simulat.,vol.17,pp.1813-1823,2014.
[20]Y.P.Pan,T.R.Sun,and H.Y.Y,Composite adaptive dynamic surface control using online recorded data,International Journal of Robust and Nonlinear Control,Doi:DOI10.1109/TNNLS.2016.2527501.
[21]Y.P.Pan,H.Y.Yu,and T.R.Sun,Global asymptotic stabilization using adaptive fuzzy PD control,IEEE transactions on cybernetics,vol.45,no.3,pp.574-582,2015.
[22]S.H.Yu,X.H.Yu,B.J.Shirinzadeh,Z.H.Mau,Continuous finite-time control for robotic manipulators with terminal sliding mode,Automatica,vol.41,pp.1957-1964,2005.
[2]R.Rakkiyappan,G.Velmurugan,and J.D.Cao,Stability analysis of fractional-order complex-valued neural networks with time delays,Chaos,Solitons&Fractals,vol.78,pp.297–316,2015.
[3]S.Pei,J.Shyu,Y.Huang,and C.Chan,Improved methods for the design of variable fractional-delay IIR digital filters,IEEE Trans.Circuits Syst.I,Reg.Papers,vol.59,no.5,pp.989-1000,2012.
[4]M.O.Efe,Fractional fuzzy adaptive sliding-mode control of a 2-DOF direct-drive robot arm,IEEE Transactions on Systems,Man,and Cybernetics,vol.38,no.6,pp.1561-1570,2008.
[5]A.H.Nayfeh,D.T.Mook,Nonlinear oscillations,Wiley Inter Science,New York,1995.
[6]E.H.Dowell,Non-linear oscillator models in bluff body aeroelasticity,Journal of Sound and Vibration,vol.75,pp.251-264,1981.
[7]B.vander Pol,J.vander Mark,Frequency demultiplication,Nature,vol.120,pp.363-364,1927.
[8]E.Domany,O.V.Gendelman,Dynamic responses and mitigation of limit cycle oscillations in Van der Pol-Duffing oscillator with nonlinear energy sink,Journal of Sound and Vibration,vol.21,pp.5489-5507,2013.
[9]Y.S.Lee,A.FVakakis,L.A.Bergman,D.M.Mc Farland,Suppression of limit cycle oscillations in the Van der Pol oscillator by means of passive nonlinear energy sinks(NESs),Structural Control and Health Monitoring,vol.13,pp.41-75,2006.
[10]O.V.Gendelman,T.Bar,Bifurcations of self-excitation regimes in a Van der Pol oscillator with a nonlinear energy sink,Physica D,vol.239,pp.220-229,2010.
[11]J.A.Dunnmon,S.C.Stanton,B.P.Mann,et al.,Power extraction from aeroelastic limit cycle oscillations,Journal of Fluids and Structures,vol.27,pp.1182-1198,2011.
[12]A.Drachinsky,D.E.Raveh,Limit-cycle oscillations of a pretensed membrane strip,Journal of Fluids and Structures,vol.60,pp.1-22,2016.
[13]M.Dardel,F.Bakhtiari-Nejad,A reduced order of complete aeroelastic model for limit cycle oscillations,Aerospace science and technology,vol.14,pp.95-105,2010.
[14]S.A.Eftekhari,F.Bakhtiari-Nejad,E.H.Dowell,Damage detection of an aeroelastic panel using limit cycle oscillation analysis,International Journal of Non-Linear Mechanics,vol.58,pp.99-110,2014.
[15]N.G.Bhoir,S.N.Singh,Output feedback nonlinear control of an aeroelastic with unsteady aerodynamics,Aerosp.Sci.Technol.,vol.8,pp.195-205,2004.
[16]T.W.Strganac,D.E.Thompson,Identification and control of limit cycle oscillations in aeroelastic systems,J.Guid.Control Dyn.,vol.23,pp.1127-1133,2008.
[17]S.Gujjula,S.N.Singh,W.Yim,Adaptive and neural control of a wing section using leading-and trailing-edge surfaces,Aerosp.Sci.Technol.,vol.9,pp.161-171,2005.
[18]C.L Chen,C.W.Chang,H.T.Yau,Terminal sliding mode control for aeroelastic systems,Nonlinear Dyn.,vol.70,pp.2015-2026,2013.
[19]C.L.Chen,C.C.Peng,H.T.Yau,High-order sliding mode controller with backstepping design for aeroelastic systems,Commun.Nonlinear Sci.Numer.Simulat.,vol.17,pp.1813-1823,2014.
[20]Y.P.Pan,T.R.Sun,and H.Y.Y,Composite adaptive dynamic surface control using online recorded data,International Journal of Robust and Nonlinear Control,Doi:DOI10.1109/TNNLS.2016.2527501.
[21]Y.P.Pan,H.Y.Yu,and T.R.Sun,Global asymptotic stabilization using adaptive fuzzy PD control,IEEE transactions on cybernetics,vol.45,no.3,pp.574-582,2015.
[22]S.H.Yu,X.H.Yu,B.J.Shirinzadeh,Z.H.Mau,Continuous finite-time control for robotic manipulators with terminal sliding mode,Automatica,vol.41,pp.1957-1964,2005.