Abstract
This paper presents a multidisciplinary conceptual design framework for unmanned aerial vehicles based on artificial intelligence-driven analysis models. This approach leverages AIdriven analysis models that include aerodynamics, structural mass, and radar cross-section predictions to bring quantitative data to the initial design stage, enabling the selection of the most appropriate configuration from various optimized concept designs. Due to the design optimization cycle, the initial dimensions of key components such as the wing, tail, and fuselage are provided more accurately for later design activities. Simultaneously, the generated structure enables more suitable design point selection through the feedback loop within the design iteration. Therefore, in addition to reducing design costs, this approach also offers a substantial time advantage in the overall design process.
Original language | English |
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Title of host publication | AIAA SciTech Forum and Exposition, 2024 |
Publisher | American Institute of Aeronautics and Astronautics Inc, AIAA |
ISBN (Print) | 9781624107115 |
DOIs | |
Publication status | Published - 2024 |
Externally published | Yes |
Event | AIAA SciTech Forum and Exposition, 2024 - Orlando, United States Duration: 8 Jan 2024 → 12 Jan 2024 |
Publication series
Name | AIAA SciTech Forum and Exposition, 2024 |
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Conference
Conference | AIAA SciTech Forum and Exposition, 2024 |
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Country/Territory | United States |
City | Orlando |
Period | 8/01/24 → 12/01/24 |
Bibliographical note
Publisher Copyright:© 2024 by Hasan Karali.