Multifidelity optimization under uncertainty for a tailless aircraft

This paper presents a multifidelity method for optimization under uncertainty for aerospace problems. In this work, the effectiveness of the method is demonstrated for the robust optimization of a tailless aircraft that is based on the Boeing Insitu ScanEagle. Aircraft design is often affected by un...

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Bibliographic Details
Main Authors: Jasa, John (Author), Martins, Joaquim R. R. A. (Author), Chaudhuri, Anirban (Contributor), Willcox, Karen E (Contributor)
Other Authors: Massachusetts Institute of Technology. Department of Aeronautics and Astronautics (Contributor)
Format: Article
Language:English
Published: American Institute of Aeronautics and Astronautics, 2018-05-02T16:33:01Z.
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