Multiobjective Conceptual Design of an Unmanned Combat Air Vehicle

Date

2012-09-19

Author

Tekinalp, Ozan

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Design optimization of a supersonic unmanned combat air vehicle is addressed. Proper mathematical models are developed, with constraints on optimization variables and performance limits. Multiple cooling multi objective simulated annealing algorithm is used to carry out the optimization. The results demonstrate that design optimization formulation as well as the algorithms employed is effective to help designers to come up with baseline configurations.

URI

https://hdl.handle.net/11511/69532

DOI

https://doi.org/10.2514/6.2012-5532

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Department of Aerospace Engineering, Conference / Seminar

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Citation Formats

O. Tekinalp, “Multiobjective Conceptual Design of an Unmanned Combat Air Vehicle,” 2012, Accessed: 00, 2020. [Online]. Available: https://hdl.handle.net/11511/69532.