Full Envelope Dynamics Modeling and Simulation for Tail-Sitter Hybrid UAVs
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- 英文论文题名：Full Envelope Dynamics Modeling and Simulation for Tail-Sitter Hybrid UAVs
- 论文作者：Yijie Ke ; Ben M.Chen
- 英文论文作者：Yijie Ke ; Ben M.Chen ; Unmanned System Research Group ; Department of Electrical and Computer Engineering ; National University of Singapore
- 年：2017
- 作者机构：Unmanned System Research Group,Department of Electrical and Computer Engineering,National University of Singapore;
- 英文论文关键词：Dynamics modeling ; Full envelope aerodynamics ; Hybrid UAV ; Tail-sitter
- 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：V279
- 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：998k
- 原文格式：D
- 会议级别：全国
摘要
This paper presents a comprehensive modeling approach for tail-sitter hybrid UAVs featured by vertical take-off and landing(VTOL) and cruise flight capabilities. The modeling approach includes all essential components, such as full angle of attack envelope wing and fuselage aerodynamics, sideslip wind effect and actuator dynamics. A unified formulation comprising all model components is derived to constitute the core of our simulation environment. Simulation results show that our approach is effective to predict flight dynamics and can serve as the testbed for real implementations.
This paper presents a comprehensive modeling approach for tail-sitter hybrid UAVs featured by vertical take-off and landing(VTOL) and cruise flight capabilities. The modeling approach includes all essential components, such as full angle of attack envelope wing and fuselage aerodynamics, sideslip wind effect and actuator dynamics. A unified formulation comprising all model components is derived to constitute the core of our simulation environment. Simulation results show that our approach is effective to predict flight dynamics and can serve as the testbed for real implementations.
This paper presents a comprehensive modeling approach for tail-sitter hybrid UAVs featured by vertical take-off and landing(VTOL) and cruise flight capabilities. The modeling approach includes all essential components, such as full angle of attack envelope wing and fuselage aerodynamics, sideslip wind effect and actuator dynamics. A unified formulation comprising all model components is derived to constitute the core of our simulation environment. Simulation results show that our approach is effective to predict flight dynamics and can serve as the testbed for real implementations.
引文
[1]Y.Song,H.Wang,Design of flight control system for a small unmanned tilt rotor aircraft,Chinese Journal of Aeronautics,22(3):250-256,2009.
[2]E.Cetinsoy,S.Dikyar,and C.Hancer,et al,Design and construction of a novel quad tilt-wing UAV,Mechatronics,22(6):723-745,2012.
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[4]Jouav:CW-20 VTOL fixed wing UAV[Online],Available:http://www.jouav.com/index.php/Jouav/index/CW20.html,Accessed on:Feb.20,2017.
[5]A.Frank,J.Mc Grew and M.Valenti,et al,Hover,transition,and level flight control design for a single-propeller indoor airplane,in Proceedings of AIAA Guidance,Navigation and Control Conference and Exhibit,2007:6318-6335.
[6]B.Yuksek,A.Vuruskan and U.Ozdemir,et al,Transition Flight Modeling of a Fixed-Wing VTOL UAV,Journal of Intelligent and Robotic Systems,84(1-4):83-105,2016.
[7]L.R.Lustosa,F.Defay and J.M.Moschetta,Longitudinal study of a tilt-body vehicle:Modeling,control and stability analysis,in Proceedings of 2015 IEEE International Conference on Unmanned Aircraft Systems,2015:816-824.
[8]M.Puopolo,J.Jacob,Model for Longitudinal Perch Maneuvers of a Fixed-Wing Unmanned Aerial Vehicle,Journal of Aircraft,52(6):2021-2031,2015.
[9]M.S.Selig,Real-Time Flight Simulation of Highly Maneuverable Unmanned Aerial Vehicles,Journal of Aircraft,51(6):1705-1725,2014.
[10]Y.Ke,H.Yu and C.Chi,et al,A systematic design approach for an unconventional UAV J-Lion with extensible morphing wings,in:Proceedings of 12th IEEE International Conference on Control and Automation,2016:44-49.
[11]Y.Ke,K.Wang and B.M.Chen,A preliminary modeling and control framework for a hybrid UAV J-lion,in:Proceedings of International Micro Air Vechicle Competition and Conference,2016:28-34.
[12]H.Glauert,Airplane propellers,in Aerodynamic theory,W.F.Durand,Eds.Heidelberg:Springer-Verlag,1935:169-360.
[13]R.G.Loewy,A two-dimensional approximation to the unsteady aerodynamics of rotary wings,Journal of the Aeronautical Sciences,24(2):81-92,2012.
[14]G.Gaonkar,D.Peters,Review of dynamic inflow modeling for rotorcraft flight dynamics,in Proceedings of 27th Structures,Structural Dynamics and Materials Conference,1988:845-871.
[15]W.Johnson,Milestones in Rotorcraft Aeromechanics,Journal of the American Helicopter Society,56(3):1-24,2011.
[16]J.R.Raol,J.Singh,Flight mechanics modeling and analysis,Boca Raton:CRC Press,2009,chapter 9.
[17]J.B.Brandt,R.W.Deters,G.K.Ananda,and M.S.Selig,UIUC Propeller Database[Online],Available:http://mselig.ae.illinois.edu/props/prop DB.html,Accessed on:Sep.1,2016.
[18]APC propeller performance data[Online],Available:http://www.apcprop.com/Articles.asp?ID=270,Accessed on:Sep.1,2016.
[19]M.S.Selig,J.J.Guglielmo,A.P.Broeren,and P.Gigure,Summary of low-speed airfoil data,Virginia Beach:Soar Tech Publications,1995.
[20]Lindenburg C,Stall coefficients:aerodynamic airfoil coefficients at large angles of attack,ECN Wind Energy,the Netherlands,ECN-RX-01-004,2001.
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[22]D.A.Spera,Models of lift and drag coefficients of stalled and unstalled airfoils in wind turbines and wind tunnels[Online],Available:https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/20090001311.pdf,Accessed on:Feb.20,2017.
[2]E.Cetinsoy,S.Dikyar,and C.Hancer,et al,Design and construction of a novel quad tilt-wing UAV,Mechatronics,22(6):723-745,2012.
[3]R.H.Stone,Control and guidance for a tail-sitter unmanned air vehicle,in Field and Service Robotics,P.Corke,S.Sukkariah,Eds.Heidelberg:Springer-Verlag,2006:453-464.
[4]Jouav:CW-20 VTOL fixed wing UAV[Online],Available:http://www.jouav.com/index.php/Jouav/index/CW20.html,Accessed on:Feb.20,2017.
[5]A.Frank,J.Mc Grew and M.Valenti,et al,Hover,transition,and level flight control design for a single-propeller indoor airplane,in Proceedings of AIAA Guidance,Navigation and Control Conference and Exhibit,2007:6318-6335.
[6]B.Yuksek,A.Vuruskan and U.Ozdemir,et al,Transition Flight Modeling of a Fixed-Wing VTOL UAV,Journal of Intelligent and Robotic Systems,84(1-4):83-105,2016.
[7]L.R.Lustosa,F.Defay and J.M.Moschetta,Longitudinal study of a tilt-body vehicle:Modeling,control and stability analysis,in Proceedings of 2015 IEEE International Conference on Unmanned Aircraft Systems,2015:816-824.
[8]M.Puopolo,J.Jacob,Model for Longitudinal Perch Maneuvers of a Fixed-Wing Unmanned Aerial Vehicle,Journal of Aircraft,52(6):2021-2031,2015.
[9]M.S.Selig,Real-Time Flight Simulation of Highly Maneuverable Unmanned Aerial Vehicles,Journal of Aircraft,51(6):1705-1725,2014.
[10]Y.Ke,H.Yu and C.Chi,et al,A systematic design approach for an unconventional UAV J-Lion with extensible morphing wings,in:Proceedings of 12th IEEE International Conference on Control and Automation,2016:44-49.
[11]Y.Ke,K.Wang and B.M.Chen,A preliminary modeling and control framework for a hybrid UAV J-lion,in:Proceedings of International Micro Air Vechicle Competition and Conference,2016:28-34.
[12]H.Glauert,Airplane propellers,in Aerodynamic theory,W.F.Durand,Eds.Heidelberg:Springer-Verlag,1935:169-360.
[13]R.G.Loewy,A two-dimensional approximation to the unsteady aerodynamics of rotary wings,Journal of the Aeronautical Sciences,24(2):81-92,2012.
[14]G.Gaonkar,D.Peters,Review of dynamic inflow modeling for rotorcraft flight dynamics,in Proceedings of 27th Structures,Structural Dynamics and Materials Conference,1988:845-871.
[15]W.Johnson,Milestones in Rotorcraft Aeromechanics,Journal of the American Helicopter Society,56(3):1-24,2011.
[16]J.R.Raol,J.Singh,Flight mechanics modeling and analysis,Boca Raton:CRC Press,2009,chapter 9.
[17]J.B.Brandt,R.W.Deters,G.K.Ananda,and M.S.Selig,UIUC Propeller Database[Online],Available:http://mselig.ae.illinois.edu/props/prop DB.html,Accessed on:Sep.1,2016.
[18]APC propeller performance data[Online],Available:http://www.apcprop.com/Articles.asp?ID=270,Accessed on:Sep.1,2016.
[19]M.S.Selig,J.J.Guglielmo,A.P.Broeren,and P.Gigure,Summary of low-speed airfoil data,Virginia Beach:Soar Tech Publications,1995.
[20]Lindenburg C,Stall coefficients:aerodynamic airfoil coefficients at large angles of attack,ECN Wind Energy,the Netherlands,ECN-RX-01-004,2001.
[21]J.D.Anderson,Fundamentals of aerodynamics,Columbus:Tata Mc Graw-Hill Education,2010.
[22]D.A.Spera,Models of lift and drag coefficients of stalled and unstalled airfoils in wind turbines and wind tunnels[Online],Available:https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/20090001311.pdf,Accessed on:Feb.20,2017.