Micro Aerial Vehicle Design Optimization using Mixed Discrete and Continuous Variables
2006 (English)In: A collection of technical papers : 11th AIAAA/ISSMO Multidisciplinary Analysis and Optimization Conferences, Reston, Virginia, USA: American Institute of Aeronautics and Astronautics, 2006, 1277-1290 p.Conference paper (Refereed)
Micro or mini aerial vehicles are characterized by the fact that they are likely to be build in relatively low numbers for the sensors and equipment available at the time of deployment. Therefore "design and build on demand" is very attractive, where a modular concept with a more or less automated design process is desirable. In this paper design automation of a Micro or Mini Aerial Vehicle (MAV) is demonstrated using design optimization with both discrete and continuous variables. This involves both selections of components for the propulsion system, as well as geometrical parameters for the airframe.
Place, publisher, year, edition, pages
Reston, Virginia, USA: American Institute of Aeronautics and Astronautics, 2006. 1277-1290 p.
Engineering and Technology
IdentifiersURN: urn:nbn:se:liu:diva-43957Local ID: 75231ISBN: 978-156347823-9OAI: oai:DiVA.org:liu-43957DiVA: diva2:264818
11th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, Portsmouth, Virginia, 6-8 September, 2006