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Design Methodology of a Hybrid Propulsion Driven Electric Powered Miniature Tailsitter Unmanned Aerial Vehicle

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Abstract

Contrary to the manned tailsitter aircraft concepts, which have been shelved and forgotten after mid 1960’s, the unmanned versions of these concepts have become popular. Since, tailsitter type UAVs combine both vertical takeoff and landing (VTOL) operation and relatively high speed cruise flight capabilities which provide manifest advantages over the other VTOL aircraft concepts, including helicopters and organic air vehicles (OAVs). However, there is no mini class tailsitter UAV with efficient high speed cruise flight capability. This paper presents the design methodology and optimization of ITU Tailsitter UAV concept with hybrid propulsion system approach to fill that gap. The initial design and analysis show the advantageous performance over other mini-class VTOL UAVs.

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References

  1. University of Sydney: T-wing Tailsitter UAV webpage. http://www.aeromech.usyd.edu.au/uav/twing/. Accessed 20 Jan 2009 (2006)

  2. Mayers, G.C., Gessow, A.: Aerodynamics of the Helicopter, 8th edn. Frederick Ungar, New York (1985)

    Google Scholar 

  3. Asson, K., Dunn, P.: Compact dynamometer system that can accurately determine propeller performance. J. Aircr. 29(1), 8–9 (1992)

    Article  Google Scholar 

  4. Ates, S., Bayezit, I., Inalhan, G.: Design and hardware-in-the-loop integration of a UAV microavionics system in a manned—unmanned joint airspace flight network simulator. J. Intell. Robot. Syst. 54(1–3), 359–386 (2009)

    Article  Google Scholar 

  5. Bass, R.M.: Small scale wind tunnel testing of model propellers. In: Aerospace Sciences Meeting, 24th, Reno, NV (1986)

  6. Beard, R., Kingston, D., Quigley, M., Snyder, D., Christiansen, R., Johnson, W., McLain, T., Goodrich, M.: Autonomous vehicle technologies for small fixed wing UAVs. AIAA J. Aerosp. Comput. Inf. Commun. 2(1), 92–108 (2005)

    Article  Google Scholar 

  7. Esteco: Esteco modefrontier official webpage. http://www.esteco.com/ (2009)

  8. Electric Ducted Fans: Ductedans.com online store. http://www.ductedfans.com/impellers_ducted_fans.html. Accessed 20 Jan 2009 (2009)

  9. Hepperle, M.: Javaprop software. http://www.mh-aerotools.de/airfoils/javaprop.htm (2006)

  10. Hepperle, M.: Javaprop software validation tests. http://www.mh-aerotools.de/airfoils/jp_validation.htm (2008)

  11. Hobby-Lobby International Inc.: Electric ducted fans. http://www.hobby-lobby.com/ductfan.htm. Retrieved 20 Jan 2009 (2009)

  12. Schuebeler Jets: Schuebeler ds51 wind tunnel test. http://www.schuebeler-jets.com/images/stories/vergleich_windkanal2.jpg. Retrieved 20 Jan 2009 (2009)

  13. Knoebel, N., Osborne, S., Snyder, D., McLain, T., Beard, R., Eldredge, A.: Preliminary modeling, control, and trajectory design for miniature autonomous tailsitters. AIAA Guidance, Navigation, and Control Conference and Exhibit (2006)

  14. Knoebel, N.B.: Adaptive quaternion control of a miniature tailsitter UAV. Ph.D. thesis, Brigham Young University (2007)

  15. Merchant, M.P., Miller, L.S.: Propeller performance measurement for low Reynolds number UAV applications. AIAA 1127, 2006 (2006)

    Google Scholar 

  16. Torres, G.E., Mueller, T.J., Srull, D.W.: Introduction to the Design of Fixed-Wing Micro Aerial Vehicles, chap. eee., pp. 39–107. AIAA (2006)

  17. Raymer, D.P.: Aircraft Design: A Conceptual Approach, chap. Aerodynamics, 2nd edn., pp. 280–288. American Institute of Aeronautics and Astronautics, New York (1992)

    Google Scholar 

  18. Shkarayev, S., Moschetta, J.M., Bataille, B.: Aerodynamic design of micro air vehicles for vertical flight. J. Aircr. 45(5), 1715–1724 (2008)

    Article  Google Scholar 

  19. Stefko, G.L., Bober, L.J., Neumann, H.E.: New Test Techniques and Analytical Procedures for Understanding the Behavior of Advanced Propellers. NTIS, Springfield, VA (USA), 24 (1983)

    Google Scholar 

  20. Stinton, D.: The Design of the Aeroplane, chap. Reciprocating Engines, pp. 308–310. BSP Professional, Oxford (1993)

    Google Scholar 

  21. Stone, R.H.: The T-wing tail-sitter research UAV. In: International Powered Lift Conference, Williamsburg, Virginia (2002)

  22. Theodorsen, T., Stickle, G.W., Brevoort, M.J., Langley Aeronautical Laboratory: Characteristics of six propellers including the high-speed range. National Advisory Committee for Aeronautics (1937)

  23. Wood, D.H., NACA, Langley Research Center: Full-scale tests of metal propellers at high tip speeds. National Advisory Committee for Aeronautics, Washington, DC (1932)

    Google Scholar 

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Authors and Affiliations

  1. Controls and Avionics Lab, Faculty of Aeronautics and Astronautics, Istanbul Technical University, Istanbul, Turkey

    Mirac Aksugur & Gokhan Inalhan

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  1. Mirac Aksugur
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  2. Gokhan Inalhan
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Correspondence to Mirac Aksugur.

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Aksugur, M., Inalhan, G. Design Methodology of a Hybrid Propulsion Driven Electric Powered Miniature Tailsitter Unmanned Aerial Vehicle. J Intell Robot Syst 57, 505–529 (2010). https://doi.org/10.1007/s10846-009-9368-0

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  • DOI: https://doi.org/10.1007/s10846-009-9368-0

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