| Title of Article |
Surrogate-assisted optimization for UAV wing preliminary design using evolutionary algorithms |
| Date of Acceptance |
2 August 2019 |
| Journal |
| Title of Journal |
Defence Technology Academic Journal |
| Standard |
OTHER (วารสารและนิตยสารทางการทหาร ) |
| Institute of Journal |
สถาบันเทคโนโลยีป้องกันประเทศ |
| ISBN/ISSN |
|
| Volume |
1 |
| Issue |
2 |
| Month |
August |
| Year of Publication |
2019 |
| Page |
46-57 |
| Abstract |
The paper demonstrates using a Kriging surrogate model in combination with evolutionary algorithms for optimizing an unmanned aerial vehicle (UAV) wing. The design problem is set to minimize wing mass subject to aeroelastic and structural design constraints. Design variables determine thicknesses and positions of wing ribs, spars and skins. Numerical results show that the Kriging model can accurately predict aeroelastic characteristics but somewhat inefficient for prediction of stress and displace. Nevertheless, this study paves the way for further improvement of the preliminary design process of an aircraft wing. |
| Keyword |
UAV design, wing optimization, aero-elasticity, aircraft wing, evolutionary algorithm |
| Author |
|
| Reviewing Status |
มีผู้ประเมินอิสระ |
| Status |
ตีพิมพ์แล้ว |
| Level of Publication |
ชาติ |
| citation |
false |
| Part of thesis |
true |
| Attach file |
|
| Citation |
0
|
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Publication
Journal Publication
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