The Multiple Cooling Multi-Objective Simulated Annealing Algorithm is used for
the conceptual design optimization of a supersonic Unmanned Combat Aerial
Vehicle (UCAV). Single and multiobjective optimization problems are addressed
while limiting performance requirements between desired bounds to obtain
viable aircraft configurations. A conceptual aircraft design code was prepared for
planned but flexible combat missions. The results demonstrate that the
optimization technique employed is an effective tool for the conceptual design of
aircrafts.
| Identifer | oai:union.ndltd.org:METU/oai:etd.lib.metu.edu.tr:http://etd.lib.metu.edu.tr/upload/12610428/index.pdf |
| Date | 01 February 2009 |
| Creators | Cavus, Nesrin |
| Contributors | Tekinalp, Ozan |
| Publisher | METU |
| Source Sets | Middle East Technical Univ. |
| Language | English |
| Detected Language | English |
| Type | M.S. Thesis |
| Format | text/pdf |
| Rights | To liberate the content for public access |
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