$\require{mediawiki-texvc}$

연합인증

연합인증 가입 기관의 연구자들은 소속기관의 인증정보(ID와 암호)를 이용해 다른 대학, 연구기관, 서비스 공급자의 다양한 온라인 자원과 연구 데이터를 이용할 수 있습니다.

이는 여행자가 자국에서 발행 받은 여권으로 세계 각국을 자유롭게 여행할 수 있는 것과 같습니다.

연합인증으로 이용이 가능한 서비스는 NTIS, DataON, Edison, Kafe, Webinar 등이 있습니다.

한번의 인증절차만으로 연합인증 가입 서비스에 추가 로그인 없이 이용이 가능합니다.

다만, 연합인증을 위해서는 최초 1회만 인증 절차가 필요합니다. (회원이 아닐 경우 회원 가입이 필요합니다.)

연합인증 절차는 다음과 같습니다.

최초이용시에는
ScienceON에 로그인 → 연합인증 서비스 접속 → 로그인 (본인 확인 또는 회원가입) → 서비스 이용

그 이후에는
ScienceON 로그인 → 연합인증 서비스 접속 → 서비스 이용

연합인증을 활용하시면 KISTI가 제공하는 다양한 서비스를 편리하게 이용하실 수 있습니다.

Design, development and ground testing of hingeless elevons for MAV using piezoelectric composite actuators

Advances in aircraft and spacecraft science, v.2 no.3, 2015년, pp.303 - 328  

Dwarakanathan, D. (Dynamics and Adaptive Structures, Structural Technologies Division, CSIR-National Aerospace Laboratories) ,  Ramkumar, R. (Dynamics and Adaptive Structures, Structural Technologies Division, CSIR-National Aerospace Laboratories) ,  Raja, S. (Dynamics and Adaptive Structures, Structural Technologies Division, CSIR-National Aerospace Laboratories) ,  Rao, P. Siva Subba (Dynamics and Adaptive Structures, Structural Technologies Division, CSIR-National Aerospace Laboratories)

Abstract AI-Helper 아이콘AI-Helper

A design methodology is presented to develop the hingeless control surfaces for MAV using adhesively bonded Macro Fiber Composite (MFC) actuators. These actuators have got the capability to deflect the trailing edge surfaces of the wing to attain the required maneuverability, besides achieving the s...

주제어

참고문헌 (31)

  1. Barbarino, S., Bilgen, O., Ajaj, R.M., Friswell, M.I. and Inman, D.J. (2011), "A review of morphing aircraft", J. Intel. Mater. Syst. Struct., 22(9), 823-877. 

  2. Barbarino, S., Saavedra Flores, E.L., Ajaj, R.M., Dayyani, I. and Friswell, M.I. (2014), "A review on shape memory alloys with applications to morphing aircraft", Smart Mater. Struct., 23(6), 063001.. 

  3. Bilgen, O., Butt, L.M., Day, S.R., Sossi, C.A., Weaver, J.P., Wolek, A., Mason, W.H. and Inman, D.J. (2013), "A novel unmanned aircraft with solid-state control surfaces: analysis and flight demonstration", J. Intel. Mater. Syst. Struct., 24(2), 147-167. 

  4. Bilgen, O. and Friswell, M.I. (2014), "Piezoceramic composite actuators for a solid-state variable-camber wing", J. Intel. Mater. Syst. Struct., 25(7), 806-817. 

  5. Bilgen, O., Kochersberger, K., Diggs, E.C., Kurdila, A.J. and Inman, D.J. (2007), "Morphing wing micro-air-vehicles via macro-fiber-composite actuators", AIAA 2007-1785, 48thAIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, Honolulu, Hawaii, April. 

  6. Bilgen, O., Kochersberger, K.B., Inman, D.J. and Ohanian, O.J. (2010), "Lightweight High Voltage Electronic Circuits for Piezoelectric Composite Actuators", J. Intel. Mater. Syst. Struct., 21(14), 1417-1426. 

  7. Bisplinghoff, R.L., Ashley, H. and Halfman, R.L. (2013), Aeroelasticity, Courier Dover Publications 

  8. Bradley, L. and Peter, I. (2012), "Finite Element Modeling of Macro Fiber Composite Piezoelectric Actuators on Micro Air Vehicles", AIAA2012-1903, 53rdAIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, Honolulu, Hawaii, April. 

  9. Bradley, W.L. and Peter, I. (2013), "A Study of Substrate Materials for Use in Conjunction with Macro Fiber Composites", AIAA2013-1916, 54thAIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, Boston, Massachusetts, USA, April. 

  10. Cote, F., Masson, P., Mrad, N. and Cotoni, V. (2004), "Dynamic and static modelling of piezoelectric composite structures using a thermal analogy with MSC/NASTRAN", Compos. Struct., 65(3-4), 471-484. 

  11. Deraemaeker, A., Nasser, H., Benjeddou, A. and Preumont, A. (2009), "Mixing rules for the piezoelectric properties of macro fiber composites", J. Intel. Mater. Syst. Struct., 20(12), 1475-1482. 

  12. Gomez, J.C. and Garcia, E. (2011), "Morphing unmanned aerial vehicles", Smart Mater. Struct., 20(10), 103001.. 

  13. Kuder, I.K., Arrieta, A.F., Raither, W.E. and Ermanni, P. (2013), "Variable stiffness material and structural concepts for morphing applications", Prog. Aerospace Sci., 63, 33-55. 

  14. LaCroix, B.W. and Ifju, P.G. (2012), "Utilization and performance enhancements of multiple piezoelectric actuators on micro air vehicles", AIAA 2012-0392, 50thAIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, Nashville, Tennessee, USA, January. 

  15. MSC Nastran (2012), "Linear Static Analysis User's Guide", MSC Software Inc, USA. 

  16. Ohanian, O.J., Hickling, C., Stiltner, B., Karni, E.D., Kochersberger, K.B., Probst, T., Gelhausen, P.A. and Blain, A.P. (2012), "Piezoelectric morphing versus servo-actuated MAV control surfaces", AIAA 2012-1512, 53rdAIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, Honolulu, Hawaii, April. 

  17. Osgar, O., Brian, D., Seth, T., Kevin, K., Troy, P., Paul, G. and Jonathon, C. (2013), "Piezoelectric morphing versus servo-actuated MAV control surfaces, Part II: flight testing", AIAA 2013-0767, 51stAIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, Grapevine (Dallas/Ft. Worth Region), Texas, USA, January. 

  18. Pankonien, A. and Inman, D.J. (2013), "Experimental testing of spanwise morphing trailing edge concept", Proc. SPIE 8688, 868815, April 10, 2013, Active and Passive Smart Structures and Integrated Systems 2013, San Diego, California, USA. 

  19. Paradies, R. and Ciresa, P. (2009), "Active wing design with integrated flight control using piezoelectric macro fiber composites", Smart Mater. Struct., 18(3), 035010. 

  20. Pelletier, A. and Mueller, T.J. (2000), "Low Reynolds number aerodynamics of low-aspect-ratio, thin/flat/cambered-plate wings", J. Aircraft., 37(5), 825-832. 

  21. Probst, T.A., Kochersberger, K., Stiltner, B., Hickling, C.J., Ohanian Iii, O.J., Karni, E., Olien, C. and Blain, A.P. (2012), "Smart material actuators as a means of UAV flight control", AIAA 2012-0486, 50thAIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, Nashville, Tennessee, USA, January. 

  22. Rodden, W.P. and Johnson, E.H. (1994), MSC/NASTRAN aeroelastic analysis: user's guide; Version 68, MacNeal-Schwendler Corporation. 

  23. Roshan Antony, Suraj, C.S. and Sankara Narayanan, S. (2011), Design of Black Kite Micro Air Vehicle, PD PR 1121, CSIR-National Aerospace Laboratories, Bangalore. 

  24. Sadraey, M.H. (2012), Aircraft Design: A Systems Engineering Approach, John Wiley & Sons. 

  25. Sanders, B., Eastep, F.E. and Forster, E. (2003), "Aerodynamic and Aeroelastic Characteristics of Wings with Conformal Control Surfaces for Morphing Aircraft", J. Aircraft., 40(1), 94-99. 

  26. Sofla, A.Y.N., Meguid, S.A., Tan, K.T. and Yeo, W.K. (2010), "Shape morphing of aircraft wing: Status and challenges", Mater. Des., 31(3), 1284-1292. 

  27. Vale, J., Leite, A., Lau, F. and Suleman, A. (2011), "Aero-structural optimization and performance evaluation of a morphing wing with variable span and camber", J. Intel. Mater. Syst. Struct., 22(10), 1057-1073. 

  28. Weisshaar, T.A. (2013), "Morphing aircraft systems: historical perspectives and future challenges", J. Aircraft., 50(2), 337-353. 

  29. Wickramasinghe, V., Chen, Y., Martinez, M., Wong, F. and Kernaghan, R. (2011), "Design and verification of a smart wing for an extreme-agility micro-air-vehicle", Smart Mater. Struct., 20(12), 125007. 

  30. ANSYS Fluent Theory Guide (2011), Release 14.0, ANSYS Inc, Southpointe, Canonsburg, PA, 15317, November. 

  31. Macro Fiber Composite - MFC, Smart Material Corp., www.smart-material.com. 

섹션별 컨텐츠 바로가기

AI-Helper ※ AI-Helper는 오픈소스 모델을 사용합니다.

AI-Helper 아이콘
AI-Helper
안녕하세요, AI-Helper입니다. 좌측 "선택된 텍스트"에서 텍스트를 선택하여 요약, 번역, 용어설명을 실행하세요.
※ AI-Helper는 부적절한 답변을 할 수 있습니다.

선택된 텍스트

맨위로