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
Link To Document :
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