Co-simulation and Experimental Study for Wingspan of Flapping Wing Micro Aerial Vehicle
The 3D model of flapping wing mechanism and veins is constructed in 3D computer aided design （CAD） software UG. Then the co-simulation model is established by using multibody dynamics software ADAMS and MATLAB. The validation of this co-simulation model is verified by comparing the simulation result...
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| Published in | Shanghai jiao tong da xue xue bao Vol. 14; no. 2; pp. 252 - 256 |
|---|---|
| Main Author | |
| Format | Journal Article |
| Language | English |
| Published |
Heidelberg
Shanghai Jiaotong University Press
01.04.2009
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| Subjects | |
| Online Access | Get full text |
| ISSN | 1007-1172 1995-8188 |
| DOI | 10.1007/s12204-009-0252-7 |
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| Abstract | The 3D model of flapping wing mechanism and veins is constructed in 3D computer aided design （CAD） software UG. Then the co-simulation model is established by using multibody dynamics software ADAMS and MATLAB. The validation of this co-simulation model is verified by comparing the simulation results with final experiments. The simulation results and experiments reveal that the relation between flapping frequency and driving voltage of motor is approximately linear under various wingspans. The variance of flapping frequency among different wingspans augments gradually with increasing voltage. Furthermore, the simulation results suggest that flapping frequency is sensitive to wingspan and decreases with increasing wingspan of veins, and the relation between flapping frequency and moment of inertia of veins is also approximately linear for various voltages. |
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| AbstractList | The 3D model of flapping wing mechanism and veins is constructed in 3D computer aided design （CAD） software UG. Then the co-simulation model is established by using multibody dynamics software ADAMS and MATLAB. The validation of this co-simulation model is verified by comparing the simulation results with final experiments. The simulation results and experiments reveal that the relation between flapping frequency and driving voltage of motor is approximately linear under various wingspans. The variance of flapping frequency among different wingspans augments gradually with increasing voltage. Furthermore, the simulation results suggest that flapping frequency is sensitive to wingspan and decreases with increasing wingspan of veins, and the relation between flapping frequency and moment of inertia of veins is also approximately linear for various voltages. The 3D model of flapping wing mechanism and veins is constructed in 3D computer aided design (CAD) software UG. Then the co-simulation model is established by using multibody dynamics software ADAMS and MATLAB. The validation of this co-simulation model is verified by comparing the simulation results with final experiments. The simulation results and experiments reveal that the relation between flapping frequency and driving voltage of motor is approximately linear under various wingspans. The variance of flapping frequency among different wingspans augments gradually with increasing voltage. Furthermore, the simulation results suggest that flapping frequency is sensitive to wingspan and decreases with increasing wingspan of veins, and the relation between flapping frequency and moment of inertia of veins is also approximately linear for various voltages. |
| Author | 彭松林 陈文元 张卫平 |
| AuthorAffiliation | Institute of Micro and Nano Science and Technology, Shanghai Jiaotong University, Shanghai 200030, China |
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| Cites_doi | 10.1016/S0924-4247(00)00527-6 10.2514/2.2807 10.1016/j.paerosci.2003.04.001 10.2514/6.2001-127 10.1242/jeb.00663 |
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| References_xml | – reference: Grasmeyer J M, Keennon M T. Development of the black widow micro air vehicle [C]// 39th AIAA Aerospace Sciences Meeting and Exhibit. Revo, NV:[s.n.], 2001: 1–9. – reference: SaneS. P.The aerodynamics of insect flight [J]The Journal of Experimental Biology2003206234191420810.1242/jeb.00663 – reference: Nick Pornsin-sirirakT.TaiY. C.NassefH.Titanium-alloy MEMS wing technology for a micro aerial vehicle application [J]Sensors and Actuators. A: Physical2001891–29510310.1016/S0924-4247(00)00527-6 – reference: Pornsin-sisirakT.LeeS. W.NassefH.MEMS wing technology for a battery-powered ornithopter [C]Thirteenth IEEE International Conference on Micro Electro Mechanical Systems2000Miyazaki, JapanIEEE79980410.1109/MEMSYS.2000.838620 – reference: Thomas J P, Qidwai M A, Matic P, et al. Composite materials with multifunctional structure-power capabilities [C]// Proc American Soc Composites 16th Technical Conf. Blacksburg, VA: [s.n.], 2001. – reference: GreekD.Prototype for a micro air vehicle [J]Prof Eng1999121126 – reference: HoS.NassefH.PornsinsirirakN.Unsteady aerodynamics and flow control for flapping wing flyers [J]Progress in Aerospace Sciences200339863568110.1016/j.paerosci.2003.04.001 – reference: GomesL.It’s a bird!It’s a spy plane!—Pentagon funds research into robin-sized robots [J]Wall Street J1999695103 – reference: AvadhanulaS.WoodR. J.SteltzE.Lift force improvements for the micromechanical flying insect[C]International Conference on Intelligent Robots and Systems2003Las VegasIEEE13501356 – reference: Gad-el-hakM.Micro-air-vehicles: Can they be controlled better? [J]J Aircraft200138341942910.2514/2.2807 – ident: 252_CR2 – start-page: 799 volume-title: Thirteenth IEEE International Conference on Micro Electro Mechanical Systems year: 2000 ident: 252_CR8 – volume: 89 start-page: 95 issue: 1–2 year: 2001 ident: 252_CR9 publication-title: Sensors and Actuators. A: Physical doi: 10.1016/S0924-4247(00)00527-6 – volume: 38 start-page: 419 issue: 3 year: 2001 ident: 252_CR3 publication-title: J Aircraft doi: 10.2514/2.2807 – volume: 6 start-page: 95 year: 1999 ident: 252_CR5 publication-title: Wall Street J – volume: 39 start-page: 635 issue: 8 year: 2003 ident: 252_CR6 publication-title: Progress in Aerospace Sciences doi: 10.1016/j.paerosci.2003.04.001 – ident: 252_CR1 doi: 10.2514/6.2001-127 – start-page: 1350 volume-title: International Conference on Intelligent Robots and Systems year: 2003 ident: 252_CR10 – volume: 206 start-page: 4191 issue: 23 year: 2003 ident: 252_CR7 publication-title: The Journal of Experimental Biology doi: 10.1242/jeb.00663 – volume: 12 start-page: 26 issue: 11 year: 1999 ident: 252_CR4 publication-title: Prof Eng |
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| Snippet | The 3D model of flapping wing mechanism and veins is constructed in 3D computer aided design （CAD） software UG. Then the co-simulation model is established by... The 3D model of flapping wing mechanism and veins is constructed in 3D computer aided design (CAD) software UG. Then the co-simulation model is established by... |
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| SubjectTerms | Architecture Computer Science Electrical Engineering Engineering Life Sciences Materials Science MATLAB 三维计算机辅助设计 协同仿真 实验 微型飞行器 扑翼 翼展 驱动电压 |
| Title | Co-simulation and Experimental Study for Wingspan of Flapping Wing Micro Aerial Vehicle |
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