Automation of conceptual design and modification of aircraft-type unmanned aerial vehicles using multidisciplinary optimization and evolutionary algorithms. Part 2: results and analysis
An example of practical application of the methodology of multidisciplinary optimization of the concept parameters of aircraft-type flight vehicles is considered in the form of solving the problem of modifying two existing aircraft with characteristics presented in open sources. The convergence of t...
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| Main Authors: | , , , , |
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| Format: | Article |
| Language: | English |
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Samara National Research University
2024-12-01
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| Series: | Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение |
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| Online Access: | https://journals.ssau.ru/vestnik/article/viewFile/28064/10926 |
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| _version_ | 1850114769393025024 |
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| author | V. A. Komarov O. E. Lukyanov V. H. Hoang E. I. Kurkin J. G. Quijada Pioquinto |
| author_facet | V. A. Komarov O. E. Lukyanov V. H. Hoang E. I. Kurkin J. G. Quijada Pioquinto |
| author_sort | V. A. Komarov |
| collection | DOAJ |
| description | An example of practical application of the methodology of multidisciplinary optimization of the concept parameters of aircraft-type flight vehicles is considered in the form of solving the problem of modifying two existing aircraft with characteristics presented in open sources. The convergence of the optimization problem was investigated. The results of validation of mathematical models of aerodynamics are presented by comparison with the experiment results. An assessment of the reliability of the calculation of the objective function was carried out using the example of solving the direct problem of calculating the take-off weight and flight performance characteristics of prototype aircraft and comparing the results with their real characteristics. A method for longitudinal trim of aircraft-type flight vehicles with two lifting surfaces with parameter optimization is proposed. |
| format | Article |
| id | doaj-art-aaa152a3736c4f538f09501e1211b70a |
| institution | OA Journals |
| issn | 2542-0453 2541-7533 |
| language | English |
| publishDate | 2024-12-01 |
| publisher | Samara National Research University |
| record_format | Article |
| series | Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение |
| spelling | doaj-art-aaa152a3736c4f538f09501e1211b70a2025-08-20T02:36:45ZengSamara National Research UniversityВестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение2542-04532541-75332024-12-01234486410.18287/2541-7533-2024-23-4-48-648932Automation of conceptual design and modification of aircraft-type unmanned aerial vehicles using multidisciplinary optimization and evolutionary algorithms. Part 2: results and analysisV. A. Komarov0https://orcid.org/0009-0007-9313-5754O. E. Lukyanov1https://orcid.org/0000-0003-3762-0249V. H. Hoang2https://orcid.org/0009-0001-7714-0963E. I. Kurkin3https://orcid.org/0000-0002-0893-9878J. G. Quijada Pioquinto4https://orcid.org/0000-0001-8225-1732Samara National Research UniversitySamara National Research UniversitySamara National Research UniversitySamara National Research UniversitySamara National Research UniversityAn example of practical application of the methodology of multidisciplinary optimization of the concept parameters of aircraft-type flight vehicles is considered in the form of solving the problem of modifying two existing aircraft with characteristics presented in open sources. The convergence of the optimization problem was investigated. The results of validation of mathematical models of aerodynamics are presented by comparison with the experiment results. An assessment of the reliability of the calculation of the objective function was carried out using the example of solving the direct problem of calculating the take-off weight and flight performance characteristics of prototype aircraft and comparing the results with their real characteristics. A method for longitudinal trim of aircraft-type flight vehicles with two lifting surfaces with parameter optimization is proposed.https://journals.ssau.ru/vestnik/article/viewFile/28064/10926unmanned aerial vehicleconceptdesigntakeoff weightoptimizationevolutionary algorithmaerodynamicsbalancingpenalty functionparallel computing |
| spellingShingle | V. A. Komarov O. E. Lukyanov V. H. Hoang E. I. Kurkin J. G. Quijada Pioquinto Automation of conceptual design and modification of aircraft-type unmanned aerial vehicles using multidisciplinary optimization and evolutionary algorithms. Part 2: results and analysis Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение unmanned aerial vehicle concept design takeoff weight optimization evolutionary algorithm aerodynamics balancing penalty function parallel computing |
| title | Automation of conceptual design and modification of aircraft-type unmanned aerial vehicles using multidisciplinary optimization and evolutionary algorithms. Part 2: results and analysis |
| title_full | Automation of conceptual design and modification of aircraft-type unmanned aerial vehicles using multidisciplinary optimization and evolutionary algorithms. Part 2: results and analysis |
| title_fullStr | Automation of conceptual design and modification of aircraft-type unmanned aerial vehicles using multidisciplinary optimization and evolutionary algorithms. Part 2: results and analysis |
| title_full_unstemmed | Automation of conceptual design and modification of aircraft-type unmanned aerial vehicles using multidisciplinary optimization and evolutionary algorithms. Part 2: results and analysis |
| title_short | Automation of conceptual design and modification of aircraft-type unmanned aerial vehicles using multidisciplinary optimization and evolutionary algorithms. Part 2: results and analysis |
| title_sort | automation of conceptual design and modification of aircraft type unmanned aerial vehicles using multidisciplinary optimization and evolutionary algorithms part 2 results and analysis |
| topic | unmanned aerial vehicle concept design takeoff weight optimization evolutionary algorithm aerodynamics balancing penalty function parallel computing |
| url | https://journals.ssau.ru/vestnik/article/viewFile/28064/10926 |
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