• DocumentCode
    720498
  • Title

    Optimized performance of a morphing micro air vehicle

  • Author

    Barcala-Montejano, M.A. ; Rodriguez-Sevillano, A.A. ; Crespo-Moreno, J. ; Bardera-Mora, R. ; Silva-Gonzalez, A.J.

  • Author_Institution
    E.T.S.I. Aeronaut. y del Espacio, Univ. Politec. de Madrid, Madrid, Spain
  • fYear
    2015
  • fDate
    9-12 June 2015
  • Firstpage
    794
  • Lastpage
    800
  • Abstract
    The objective of this research is to demonstrate how adaptive wings improve the overall performance of conventional micro air vehicles (MAVs). This will allow MAVs to fulfill missions with different range and endurance requirements, and therefore to perform a wider range of missions than conventional MAVs. These adaptive wings are achieved with the use of macro-fiber composites devices, a low-cost, state-of-the-art system. Moreover, a set of experimental tests at low Reynolds numbers for wings of low aspect ratio has been assessed and validated in this research.
  • Keywords
    adaptive control; aerodynamics; aerospace components; aircraft; Reynolds numbers; adaptive wings; conventional MAV; endurance requirement; macro-fiber composites device; morphing micro air vehicle; optimized performance; Aerodynamics; Aircraft; Automotive components; Performance evaluation; Shape; Vehicles; Voltage control; MAV; adaptive wings; enhanced performance; macro-fiber composites devices; morphing;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Unmanned Aircraft Systems (ICUAS), 2015 International Conference on
  • Conference_Location
    Denver, CO
  • Print_ISBN
    978-1-4799-6009-5
  • Type

    conf

  • DOI
    10.1109/ICUAS.2015.7152363
  • Filename
    7152363