• DocumentCode
    3200535
  • Title

    Systems integration in a UAS design. An example of undergraduate students´ tasks

  • Author

    Gandía-Agüera, F. ; Barcala-Montejano, M.A. ; Rodríguez-Sevillano, A.A. ; Holgado-Vicente, J.M.

  • Author_Institution
    Dept. de Aerotecnia, Univ. Politec. de Madrid, Madrid, Spain
  • fYear
    2011
  • fDate
    4-6 April 2011
  • Firstpage
    470
  • Lastpage
    476
  • Abstract
    Systems integration is the origin of most major difficulties found in the engineering design of aeronautical vehicles. The whole design team must assure that each subsystem accomplishes its particular goals and that, together with the rest of the systems, they all meet the general aircraft requirements. Design and building of UAS is a field of actuation to which leading Universities, research Centers and Aeronautical designers have dedicated a lot of effort. In recent years, a team of students, lecturers and professors at the Escuela Universitaria de Ingeniería Técnica Aeronáutica (EUITA) have been working on the design and building of a UAS for civil observation. The design of multi-mission Unmanned Aerial Vehicles (UAVs) has seen a rapid progress in the last years. A wide variety of designs and applications, some of them really ingenious, have been proposed. The project, which has been going on as a teamwork experience for the last ten years, consists of the design and building of a UAV, and its peculiarity is that it has been carried out entirely by undergraduate students, as part of their Final Research Project. The students face a challenge that includes all the features and stages of an authentic engineering project. We present the current moment of evolution in the process, together with a description of the main difficulties the project has undergone, as a global experience in engineering design and development.
  • Keywords
    aerospace computing; aircraft; control engineering computing; control engineering education; remotely operated vehicles; UAS design; UAV; aeronautical vehicle; engineering design; multimission unmanned aerial vehicle; systems integration; undergraduate student task; unmanned aircraft system; Aerodynamics; Airplanes; Buildings; Engineering education; Payloads; Servomotors; UAS design; design; experience; systems integration; undergraduate students;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Global Engineering Education Conference (EDUCON), 2011 IEEE
  • Conference_Location
    Amman
  • Print_ISBN
    978-1-61284-642-2
  • Type

    conf

  • DOI
    10.1109/EDUCON.2011.5773178
  • Filename
    5773178