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Mechanics of Multifunctional Wings with Solar Cells for Robotic Birds

  • Conference paper
Mechanics of Composite and Multi-functional Materials, Volume 7

Abstract

Inspired by nature, Flapping Wing Aerial Vehicles (FWAVs), also known as Robotic Birds, use flexible compliant wings that deform while flapping to generate the aerodynamic forces necessary for flight. These vehicles sustain short flights due to the limited payload for on-board energy storage. Using flexible solar cells, energy can be harvested during flight to extend the flight of the FWAV. By integrating flexible solar cells into the wing structure of the FWAV, more electrical power is produced but at a cost. The solar cells increase the overall mass of the vehicle while also altering the deformation of the wing. These changes to the wing ultimately have an effect on the performance of the FWAV. In this paper, three different wing designs were designed, built and tested. The Robo Raven platform was used for each wing design. The first design was the original wing design without solar cells. The second design hosted 12 solar modules integrated into the wings. The final design was composed of 22 solar modules integrated into the wings. The aerodynamic forces generated by each wing design were observed in a wind tunnel while the FWAV was attached to a six DOF load cell. To understand how the wings changed with respect to deformation each wing was also observed in the wind tunnel 3D using Digital Image Correlation (DIC). The results from DIC demonstrated a correlation between the lift and thrust forces produced by the wings and the biaxial and shear strains observed on the wings surface respectively. By observing the power output form the solar cells while flapping, the corresponding wave form correlated well to the thrust force measurements. This allows th solar cells to also behave as sensors while flying. The resulting platform, Robo Raven III, is the first ornithopter to fly while using energy harvested from solar cells.

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References

  1. Gerdes, J.W., Gupta, S.K., Wilkerson, S.: A review of bird-inspired flapping wing miniature air vehicle designs. ASME J. Mech. Robot. 4(2), 021003.1-021003.11(2012)

    Google Scholar 

  2. Kumar, V., Michael, N.: Opportunities and challenges with autonomous micro aerial vehicles. Int. J. Robot. Res.31(11), 1279-1291 (2012)

    Google Scholar 

  3. Pines, D.J., Bohorquez, F.: Challenges facing future micro-air-vehicle development. J. Aircr. 43(2), 290–305 (2006)

    Article  Google Scholar 

  4. Sane, S.P., Dickinson, M.H.: The aerodynamic effects of wing rotation and a revised quasi-steady model of flapping flight. J. Exp. Biol. 205, 1087–1096 (2002)

    Google Scholar 

  5. de Croon, G.C.H.E., de Clerq, K.M.E., Ruijsink, R., Remes, B., de Wagter, C.: Design, aerodynamics, and vision-based control of the delfly. Int. J. Micro Air Vehicles 1(2), 71–97 (2009)

    Article  Google Scholar 

  6. Muijres, F.T., Johansson, L.C., Barfield, R., Wolf, M., Spedding, G.R., Hedenstrom, A.: Leading-edge vortex improves lift in slow-flying bats. Science 319, 1250–1253 (2008)

    Article  Google Scholar 

  7. Zhao, L., Huang, Q., Deng, X., Sane, S.: Aerodynamic effects of flexibility in flapping wings. Interface, 7(44):485-97 (2009)

    Google Scholar 

  8. Arabagi, V., Hines, L., Sitti, M.: Design and manufacturing of a controllable miniature flapping wing robotic platform. Int. J. Robot. Res. 31(6), 785–800 (2012)

    Article  Google Scholar 

  9. Mahjoubi, H., Byl, K.: Trajectory tracking in the sagittal plane: decoupled lift/thrust control via tunable impedance approach in flapping-wing MAVs. American Control Conference (ACC). (2013)

    Google Scholar 

  10. Keennon, M., et al.: Development of the nano hummingbird: a tailless flapping wing micro air vehicle. Presented at 50th AIAA aerospace sciences meeting, Nashville, Tennessee 2012

    Google Scholar 

  11. Pornsin-Sirirak, T., Tai, Y., Ho, C., Keennon, M.: Microbat: a palm-sized electrically powered ornithopter. In: Proceedings of the NASA/JPL Workshop on Biomorphic Robotics, Pasadena, CA 2001

    Google Scholar 

  12. Mueller, T.J.: Fixed and flapping wing aerodynamics for micro air vehicle applications. American Institute of Aeronautics and Astronautics, Reston, VA (2001)

    Google Scholar 

  13. Yang, L.J., Hsu, C.K., Ho, J.Y., Feng, C.K.: Flapping wings with PVDF sensors to modify the aerodynamic forces of a micro aerial vehicle. Sens. Actuators, A (2007)

    Google Scholar 

  14. Hsu, C.K., Ho, J.Y., Feng, G.H., Shih, H.M., Yang, L.J.: A flapping MAV with PVDF-parylene composite skin. In: Proceedings of the Asia-Pacific Conference of Transducers and Micro-Nano Technology (2006)

    Google Scholar 

  15. Tsai, B.J., Fu, Y.C.: Design and aerodynamic analysis of a flapping-wing micro aerial vehicle. Aerosp. Sci. Technol. 13(7), 383–392 (2009)

    Article  Google Scholar 

  16. Hsu, C.K., Evans, J., Vytla, S., Huang, P.: Development of flapping wing micro air vehicles—design, CFD, experiment and actual flight. In: 48th AIAA Aerospace Sciences Meeting, Orlando, FL (2010)

    Google Scholar 

  17. Cox, A., Monopoli, D., Cveticanin, D., Goldfarb, M., Garcia, E.: The development of elastodynamic components for piezoelectrically actuated flapping micro-air vehicles. J. Intell. Mater. Syst. Struct. 13, 611–615 (2002)

    Article  Google Scholar 

  18. Yan, J., Wood, R.J., Avadhanula, S., Sitti, M., Fearing, R.S.: Towards flapping wing control for a micromechanical flying insect. In: Proceedings ICRA. IEEE International Conference on Robotics and Automation (2001)

    Google Scholar 

  19. Fenelon, M.A.A., Furukawa, T.: Design of an active flapping wing mechanism and a micro aerial vehicle using a rotary actuator. Mech. Mach. Theory (2009)

    Google Scholar 

  20. Jones, K.D., Bradshaw, C.J., Papadopoulos, J., Platzer, M.F., Improved performance and control of flapping-wing propelled micro air vehicles. In: Proceedings of the AIAA 42nd Aerospace Sciences Meeting and Exhibit, Reno, NV (2004)

    Google Scholar 

  21. Zdunich, P., Bilyk, D., MacMaster, M., Loewen, D., DeLaurier, J., Kornbluh, R., Low, T., Stanford, S., Holeman, D.: Development and testing of the mentor flapping-wing micro air vehicle. J. Aircr. 44(5), 1701–1711 (2007)

    Article  Google Scholar 

  22. Madangopal, R., Khan, Z., Agrawal, S.: Biologically inspired design of small flapping wing bird vehicles using four-bar mechanisms and quasi-steady aerodynamics. J. Mech. Des., 127(4), 809-817 (2005)

    Google Scholar 

  23. Bejgerowski, W., Ananthanarayanan, A., Mueller, D., Gupta, S.K.: Integrated product and process design for a flapping wing drive-mechanism. J. Mech. Des., 131(6), 061006 (2009)

    Google Scholar 

  24. Mueller, D., Gerdes, J.W., Gupta, S.K.: Incorporation of passive wing folding in flapping wing miniature air vehicles. ASME Mechanism and Robotics Conference, San Diego, CA (2009)

    Google Scholar 

  25. Bejgerowski, W., Gupta, S.K., Bruck, H.A.: A systematic approach for designing multifunctional thermally conducting polymer structures with embedded actuators. J. Mech. Des., 131(11), 111009-111009-8 (2009)

    Google Scholar 

  26. Gerdes, J., Holness, A., Perez-Rosado, A., Roberts, L., Greisinger, A.J.G., Barnett, E., Kempny, J., Lingam, D., Yeh, C.H., Bruck, H.A., Gupta, S.K.: Design, manufacturing, and testing of Robo Raven. Advanced Manufacturing Lab Technical Report, University of Maryland, College Park, MD (2014)

    Google Scholar 

  27. Perez-Rosado, A., Griesinger, A.J.G., Bruck, H.A., Gupta, S.K.: Performance characterization of multifunctional wings with integrated solar cells for miniature air vehicles. In: ASME 2014 International Design Engineering Technical and Computers and Information in Engineering Conference, Buffalo, NY, 2014

    Google Scholar 

  28. Gerdes, J.W., Holness, A., Perez-Rosado, A., Roberts, L., Greisinger, A., Barnett, E., Kempny, J., Lingam, D., Yeh, C.H., Bruck, H.A., Gupta, S.K.: Robo Raven: a flapping-wing air vehicle with highly compliant and independently controlled wings. Soft Robot., 1(4), 275-288 (2014)

    Google Scholar 

  29. Nemat-Nasser, S., Plaistead, T., Starr, A., Amirkhizi, A.: Multifunctional materials. In: Bar-Cohen, Y. (ed.) Biomimetics: biologically inspired technologies. CRC Press, Boca Raton, FL (2005)

    Google Scholar 

  30. Thomas, J.P., Qidwai, M.A.: The design and application of multifunctional structure-battery materials systems. JOM 57(3), 18–24 (2005)

    Article  Google Scholar 

  31. Ma, K.Y., Chirarattananon, P., Fuller, S.B., Wood, R.J.: Controlled flight of a biologically inspired, insect-scale robot. Science 340, 603–607 (2013)

    Article  Google Scholar 

  32. Thomas, J.P., et al.: Multifunctional structure-plus-power concepts., 43rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, Denver, CO (2002)

    Google Scholar 

  33. Wissman, J., Perez-Rosado, A., Edgerton, A., Levi, B.M., Karakas, Z.N., Kujawski, M., Phillips, A., Papavizas, N., Fallon, D., Bruck, H.A., Smela, E.: New compliant strain gauges for self-sensing dynamic deformation of flapping wings on miniature air vehicles. Smart Mater. Struct., 22(8), 085031 (2013)

    Google Scholar 

  34. Mueller, D., Bruck, H.A., Gupta, S.K.: Measurement of thrust and lift forces associated with drag of compliant flapping wing air micro air vehicles using a new test stand design. Exp. Mech. 50(6), 725–735 (2010)

    Article  Google Scholar 

  35. Gerdes, J.W., Roberts, L., Barnett, E., Kempny, J., Perez-Rosado, A., Bruck, H.A., Gupta, S.K.: Wing performance characterization for flapping wing air vehicles. ASME Mechanism and Robotics Conference, Portland, OR (2013)

    Google Scholar 

  36. Gerdes, J.W., Cellon, K.C., Bruck, H.A., Gupta, S.K.: Characterization of the mechanics of compliant wing designs for flapping-wing miniature air vehicles. Exp. Mech. 53(9), 1561–1571 (2013)

    Article  Google Scholar 

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Acknowledgments

This research has been supported by Dr. Byung-Lip “Les” Lee at AFOSR through grant FA95501210158. Opinions expressed in this paper are those of the authors and do not necessarily reflect opinions of the sponsors.

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Correspondence to Hugh A. Bruck .

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Perez-Rosado, A., Gupta, S.K., Bruck, H.A. (2016). Mechanics of Multifunctional Wings with Solar Cells for Robotic Birds. In: Ralph, C., Silberstein, M., Thakre, P., Singh, R. (eds) Mechanics of Composite and Multi-functional Materials, Volume 7. Conference Proceedings of the Society for Experimental Mechanics Series. Springer, Cham. https://doi.org/10.1007/978-3-319-21762-8_1

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  • DOI: https://doi.org/10.1007/978-3-319-21762-8_1

  • Publisher Name: Springer, Cham

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  • Online ISBN: 978-3-319-21762-8

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