The Aerodynamics and Compact Dynamic Model of a Flapping Wing Vehicle
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- 英文论文题名：The Aerodynamics and Compact Dynamic Model of a Flapping Wing Vehicle
- 论文作者：Chen Qian ; Yongchun Fang ; Xiao Liang
- 英文论文作者：Chen Qian ; Yongchun Fang ; Xiao Liang ; Institute of Robotics and Automatic Information System ; Nankai University ; Tianjin Key Laboratory of Intelligent Robotics ; Nankai University
- 年：2017
- 作者机构：Institute of Robotics and Automatic Information System,Nankai University;Tianjin Key Laboratory of Intelligent Robotics,Nankai University;
- 英文论文关键词：Flapping wing vehicle ; Quasi-steady ; Dynamic modeling
- 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（B）
- 英文会议录名称：Proceedings of the 36th Chinese Control Conference（B）
- 语种：英文
- 分类号：V211.5
- 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：6
- 文件大小：1208k
- 原文格式：D
- 会议级别：全国
摘要
In this paper, the dynamics of a flapping wing vehicle are studied. A quasi-steady model is developed to analyze its aerodynamic forces and moments. The unsteady effects are considered both in hovering state and forward flight state. Different from existing flapping wing vehicle dynamics model, the rudder's dynamics are concurrently considered in the proposed one.Numerical simulation is conducted for showing the detail characteristics of the flapping wing vehicle. After rigorous summation and analysis, a simplified dynamic model is constructed by using the averaging theory. The development of the simplified model paved the way for further studies and applications of similar flapping vehicle mechanism, such as perturbation analysis and controller design.
In this paper, the dynamics of a flapping wing vehicle are studied. A quasi-steady model is developed to analyze its aerodynamic forces and moments. The unsteady effects are considered both in hovering state and forward flight state. Different from existing flapping wing vehicle dynamics model, the rudder's dynamics are concurrently considered in the proposed one.Numerical simulation is conducted for showing the detail characteristics of the flapping wing vehicle. After rigorous summation and analysis, a simplified dynamic model is constructed by using the averaging theory. The development of the simplified model paved the way for further studies and applications of similar flapping vehicle mechanism, such as perturbation analysis and controller design.
In this paper, the dynamics of a flapping wing vehicle are studied. A quasi-steady model is developed to analyze its aerodynamic forces and moments. The unsteady effects are considered both in hovering state and forward flight state. Different from existing flapping wing vehicle dynamics model, the rudder's dynamics are concurrently considered in the proposed one.Numerical simulation is conducted for showing the detail characteristics of the flapping wing vehicle. After rigorous summation and analysis, a simplified dynamic model is constructed by using the averaging theory. The development of the simplified model paved the way for further studies and applications of similar flapping vehicle mechanism, such as perturbation analysis and controller design.
引文
[1]W.Shyy,H.Aono,S.K.Chimakurthi,et al.,Recent progress in flapping wing aerodynamics and aeroelasticity.Progress in Aerospace Sciences,2010,46(7):284-327.
[2]M.H.Dickinson,F.O.Lehmann and S.P.Sane,Wing rotation and the aerodynamic basis of insect flight.Science,1999,284(5422):1954-1960.
[3]W.Shyy,C.Kang,P.Chirarattananon,et al.,Aerodynamics,sensing and control of insect-scale flapping-wing flight Proc.R.Soc.A.The Royal Society,2016,472(2186):20150712.
[4]P.Zdunich,D.Bilyk,M.Macmaster,et al.,Development and Testing of the Mentor Flapping-Wing Micro Air Vehicle.Journal of Aircraft,2007,44(5):1701-1711.
[5]G.De Croon,K.M.E.De Clercq,R.Ruijsink,et al.,Design,aerodynamics,and vision-based control of the Del Fly.International Journal of Micro Air Vehicles,2009,1(2):71-97.
[6]M.Keennon,K.Klingebiel,H.Won,et al.,Development of the nano hummingbird:A tailless flapping wing micro air vehicle.AIAA aerospace sciences meeting.Reston,VA:AIAA,2012:1-24.
[7]R.J.Wood,The first takeoff of a biologically inspired atscale robotic insect.IEEE Transactions on Robotics,24,pp.341C347,2008.
[8]X.Deng,L.Schenato,W.C.Wu,et al.,Flapping flight for biomimetic robotic insects:part I-system modeling.IEEE Transactions on Robotics,2006,22(4):776-788.
[9]A.Gogulapati,P.P.Friedmann,Approximate Aerodynamic and Aeroelastic Modeling of Flapping Wings in Forward Flight.AIAA Journal,2014,52(1):212-218.
[10]C.Orlowski,A.Girard and W.Shyy,Open loop pitch control of a flapping wing micro-air vehicle using a tail and control mass[C]//Proceedings of the 2010 American Control Conference.IEEE,2010:536-541.
[11]J.P.Whitney,R.J.Wood,Aeromechanics of passive rotation in flapping flight.Journal of Fluid Mechanics,2010,660:197-220.
[12]Mahjoubi H,Byl K,Analysis of a tunable impedance method for practical control of insect-inspired flapping-wing MAVs.2011 50th IEEE Conference on Decision and Control and European Control Conference.IEEE,2011:3539-3546.
[13]K.Byl,A passive dynamic approach for flapping-wing microaerial vehicle control.ASME 2010 Dynamic Systems and Control Conference.American Society of Mechanical Engineers,2010:215-223.
[14]Jr.J.D.Anderson,Fundamentals of aerodynamics.Tata Mc Graw-Hill Education,2010.
[15]N.Yokoyama,K.Senda,M.Iima,et al.,Aerodynamic forces and vortical structures in flapping butterfly’s forward flight.Physics of Fluids(1994-present),2013,25(2):021902.
[16]H.Nagai,K.Isogai,T.Fujimoto,et al.,Experimental and numerical study of forward flight aerodynamics of insect flapping wing.AIAA Journal,2009,47(3):730-742.
[17]A.Pelletier,T.J.Mueller,Low Reynolds Number Aerodynamics of Low-Aspect-Ratio,Thin/Flat/Cambered-Plate Wings.Journal of Aircraft,2012,37(5):825-832.
[18]M.H.Dickinson,K.G.Gotz,Unsteady aerodynamic performance of model wings at low Reynolds numbers.Journal of Experimental Biology,1993,174(1):45-64.
[19]P.Mancini,F.Manar,K.Granlund,et al.,Unsteady aerodynamic characteristics of a translating rigid wing at low Reynolds number.Physics of Fluids,2015,27(12):2691-2704.
[20]Z.J.Wang,Vortex shedding and frequency selection in flapping flight.Journal of Fluid Mechanics,2000,410:323-341.
[21]M.Sun,J.Tang,Unsteady aerodynamic force generation by a model fruit fly wing in flapping motion.Journal of Experimental Biology,2002,205(1):55-70.
[22]A.Banazadeh,N.Taymourtash,Adaptive attitude and position control of an insect-like flapping wing air vehicle.Nonlinear Dynamics,2016:1-20.
[2]M.H.Dickinson,F.O.Lehmann and S.P.Sane,Wing rotation and the aerodynamic basis of insect flight.Science,1999,284(5422):1954-1960.
[3]W.Shyy,C.Kang,P.Chirarattananon,et al.,Aerodynamics,sensing and control of insect-scale flapping-wing flight Proc.R.Soc.A.The Royal Society,2016,472(2186):20150712.
[4]P.Zdunich,D.Bilyk,M.Macmaster,et al.,Development and Testing of the Mentor Flapping-Wing Micro Air Vehicle.Journal of Aircraft,2007,44(5):1701-1711.
[5]G.De Croon,K.M.E.De Clercq,R.Ruijsink,et al.,Design,aerodynamics,and vision-based control of the Del Fly.International Journal of Micro Air Vehicles,2009,1(2):71-97.
[6]M.Keennon,K.Klingebiel,H.Won,et al.,Development of the nano hummingbird:A tailless flapping wing micro air vehicle.AIAA aerospace sciences meeting.Reston,VA:AIAA,2012:1-24.
[7]R.J.Wood,The first takeoff of a biologically inspired atscale robotic insect.IEEE Transactions on Robotics,24,pp.341C347,2008.
[8]X.Deng,L.Schenato,W.C.Wu,et al.,Flapping flight for biomimetic robotic insects:part I-system modeling.IEEE Transactions on Robotics,2006,22(4):776-788.
[9]A.Gogulapati,P.P.Friedmann,Approximate Aerodynamic and Aeroelastic Modeling of Flapping Wings in Forward Flight.AIAA Journal,2014,52(1):212-218.
[10]C.Orlowski,A.Girard and W.Shyy,Open loop pitch control of a flapping wing micro-air vehicle using a tail and control mass[C]//Proceedings of the 2010 American Control Conference.IEEE,2010:536-541.
[11]J.P.Whitney,R.J.Wood,Aeromechanics of passive rotation in flapping flight.Journal of Fluid Mechanics,2010,660:197-220.
[12]Mahjoubi H,Byl K,Analysis of a tunable impedance method for practical control of insect-inspired flapping-wing MAVs.2011 50th IEEE Conference on Decision and Control and European Control Conference.IEEE,2011:3539-3546.
[13]K.Byl,A passive dynamic approach for flapping-wing microaerial vehicle control.ASME 2010 Dynamic Systems and Control Conference.American Society of Mechanical Engineers,2010:215-223.
[14]Jr.J.D.Anderson,Fundamentals of aerodynamics.Tata Mc Graw-Hill Education,2010.
[15]N.Yokoyama,K.Senda,M.Iima,et al.,Aerodynamic forces and vortical structures in flapping butterfly’s forward flight.Physics of Fluids(1994-present),2013,25(2):021902.
[16]H.Nagai,K.Isogai,T.Fujimoto,et al.,Experimental and numerical study of forward flight aerodynamics of insect flapping wing.AIAA Journal,2009,47(3):730-742.
[17]A.Pelletier,T.J.Mueller,Low Reynolds Number Aerodynamics of Low-Aspect-Ratio,Thin/Flat/Cambered-Plate Wings.Journal of Aircraft,2012,37(5):825-832.
[18]M.H.Dickinson,K.G.Gotz,Unsteady aerodynamic performance of model wings at low Reynolds numbers.Journal of Experimental Biology,1993,174(1):45-64.
[19]P.Mancini,F.Manar,K.Granlund,et al.,Unsteady aerodynamic characteristics of a translating rigid wing at low Reynolds number.Physics of Fluids,2015,27(12):2691-2704.
[20]Z.J.Wang,Vortex shedding and frequency selection in flapping flight.Journal of Fluid Mechanics,2000,410:323-341.
[21]M.Sun,J.Tang,Unsteady aerodynamic force generation by a model fruit fly wing in flapping motion.Journal of Experimental Biology,2002,205(1):55-70.
[22]A.Banazadeh,N.Taymourtash,Adaptive attitude and position control of an insect-like flapping wing air vehicle.Nonlinear Dynamics,2016:1-20.