Automation of conceptual design and modification of aircraft-type unmanned aerial vehicles using multidisciplinary optimization and evolutionary algorithms. Part 2: results and analysis


Cite item

Full Text

Abstract

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.

About the authors

V. A. Komarov

Samara National Research University

Author for correspondence.
Email: vkomarov@ssau.ru
ORCID iD: 0009-0007-9313-5754

Doctor of Science (Engineering), Professor, Director of Research and Educational Center for Aircraft Structures (REC-202)

Russian Federation

O. E. Lukyanov

Samara National Research University

Email: lukyanov.oe@ssau.ru
ORCID iD: 0000-0003-3762-0249

Candidate of Science (Engineering), Associate Professor of the Department of Aircraft Construction and Design

Russian Federation

V. H. Hoang

Samara National Research University

Email: hunghoang2508@gmail.com
ORCID iD: 0009-0001-7714-0963

Postgraduate Student of the Department of Aircraft Construction and Design

Russian Federation

E. I. Kurkin

Samara National Research University

Email: kurkin.ei@ssau.ru
ORCID iD: 0000-0002-0893-9878

Candidate of Science (Engineering), Associate Professor of the Department of Aircraft Construction and Design

Russian Federation

J. G. Quijada Pioquinto

Samara National Research University

Email: hosekihada@yandex.ru
ORCID iD: 0000-0001-8225-1732

Postgraduate Student of the Department of Aircraft Construction and Design

Russian Federation

References

  1. Komarov V.А., Lukyanov O.E., Hoang V.H., Kurkin E.I., Quijada Pioquinto J.G. Automation of conceptual design and modification of aircraft type unmanned aerial vehicles using multidisciplinary optimization and evolutionary algorithms. Part 1: Methods and models. Vestnik of Samara University. Aerospace and Mechanical Engineering. 2024. V. 23, no. 3. P. 42-57. (In Russ.). doi: 10.18287/2541-7533-2024-23-3-42-57
  2. Raymer D. Aircraft design: A conceptual approach. American Institute of Aeronautics and Astronautics, 2018. 1062 p. doi: 10.2514/4.104909
  3. Proektirovanie samoletov [Aircraft design / ed. by S.M. Eger]. Moscow: Mashinostroenie Publ., 1983. 616 p.
  4. Torenbeek E. Advanced aircraft design: Conceptual design, analysis and optimization of subsonic civil airplanes. Hoboken, New Jersey: John Wiley & Sons, 2013. 436 p.
  5. Badyagin A.A., Mukhamedov F.A. Proektirovanie legkikh samoletov [Design of light aircraft]. Moscow: Mashinostroenie Publ., 1978. 208 p.
  6. Sheynin V.M., Kozlovskiy V.I. Vesovoe proektirovanie i effektivnost' passazhirskikh samoletov. T. 1. Vesovoy raschet samoleta i vesovoe planirovanie [Weight design and efficiency of passenger aircraft. V. 1]. Moscow: Mashinostroenie Publ., 1977. 343 p.
  7. Komarov V.A., Gumeniuk A.V. Estimation of weight efficiency of the powerschemes of lift surfaces. Vestnik of the Samara State Aerospace University. 2002. No. 1. P. 45-54. (In Russ.)
  8. Komarov V.A. Weight analysis of aircraft structures: theoretical foundations. Polyot. All-Russian Scientific and Technical Journal. 2000. No. 1. P. 31-39. (In Russ.)
  9. Belotserkovskiy S.M. Tonkaya nesushchaya poverkhnost' v dozvukovom potoke gaza [Thin lifting surface in subsonic gas flow]. Moscow: Nauka Publ., 1965. 244 p.
  10. Katz J., Plotkin A. Low-speed aerodynamics: From wing theory to panel methods. McGraw-Hill, 1991. 656 p.
  11. Budziak K. Aerodynamic analysis with athena vortex lattice (AVL). Hamburg University of Applied Sciences, 2015. 72 p.
  12. AVL overview. Available at: https://web.mit.edu/drela/Public/web/avl/
  13. FreeCAD – Your own 3D parametric modeler. Available at: https://www.freecad.org/
  14. Komarov V.A., Tarasov V.V., Frolov V.A., Shakhov V.G. Wind tunnel for research and development at higher education institutes. All-Russian Scientific-Technical Journal «Polyot». 2006. No. 10. P. 34-40. (In Russ.)
  15. Lukianov O.E., Tarasova E.V., Martynova V.A. Remote management of experimental installation and utomation of processing of experimental data. Izvestiya Samarskogo nauchnogo tsentra RAN. 2017. V. 19, no. 1. P. 128-132. (In Russ.)
  16. Lukianov O.E., Martynova V.A. Exploratory tests of aerodynamic characteristics of model of the case of the bearing form. Izvestiya Samarskogo Nauchnogo Tsentra RAN. 2016. V. 18, no. 1. P. 83-89. (In Russ.)
  17. The General Atomics «Predator MQ-1» UAS. Available at: https://barnardmicrosystems.com/UAV/uav_list/predator.html
  18. Srednevysotnyy bespilotnyy letatel'nyy apparat bol'shoy prodolzhitel'nosti poleta United 40 [Medium-altitude long-endurance unmanned aerial vehicle United 40]. Available at: https://vpk.name/library/f/united-40.html
  19. Kozlov D.M., Komarov V.A. O nastroyke algoritmov sluchaynogo poiska po testovym modelyam. Sb. Materialov Vsesoyuznoy Shkoly-seminara «Avtomatizirovannoe Optimal'noe Proektirovanie Inzhenernykh Ob"Ektov i Tekhnologicheskikh Protsessov» (March, 2-9, 1974, Yoshkar-Ola). Part 1. Gor'kiy: Lobachevsky State University Publ., 1974. P. 67-70. (In Russ.)

Supplementary files

Supplementary Files
Action
1. JATS XML
Download

Copyright (c) 2024 VESTNIK of Samara University. Aerospace and Mechanical Engineering

Creative Commons License
This work is licensed under a Creative Commons Attribution-ShareAlike 4.0 International License.

This website uses cookies

You consent to our cookies if you continue to use our website.

About Cookies