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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