Design Rule Extraction Using Multi-Fidelity Surrogate Model for Unmanned Combat Aerial Vehicles
Author:
Affiliation:
1. Seoul National University, Seoul 08826, Republic of Korea
Funder
Institute for Information and Communications Technology Promotion
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.C036489
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