Parameterization of a power regression model for aircraft wing mass using a two-criteria estimation method
Аuthors
Irkutsk State Transport University (IrGUPS), 15, Chernyshevsky str., Irkutsk, 664074, Russia
e-mail: mik2178@yandex.ru
Abstract
The problem of predicting the mass of aircraft at the initial stage of their design, as well as the mass of their individual components, is a significant challenge today. There are various methods for addressing this issue, one of which is to utilize well-established «weight formulas» or to derive new relationships through regression analysis. One of the most significant structural components of large transport aircraft is the wings, and to estimate the mass of these wings various techniques have been developed including those proposed by Thorenbeck, Shevell, Howe, Kundu, Sheinin and Badyagin. Often a power function such as the Cobb-Douglas model is used to describe the relationship between wing mass and influencing factors, and it is necessary to construct a power regression model by taking the logarithm of the equation and estimating the coefficients of the resulting linear model using ordinary least squares. In this paper, we propose a previously developed two-criteria assessment method for parameterizing linear regression models. This method forms a set of Pareto-optimal alternatives, including estimates from the least squares and absolute deviation methods and other similar methods. To create the Pareto set, we solve a series of linear programming problems. We describe a specific algorithm for parameterizing power regression using this two-criterion method. Using the proposed algorithm, it was possible to improve the quality of the previously developed model of aircraft wing mass based on information about thirty-two different aircraft characteristics. In terms of mean absolute error, the improvement was approximately 31%, and in terms of root mean square error, it was 26.4%.
Keywords:
regression analysis, aircraft wing mass, power regression, two-criteria estimation method, ordinary least squares method, least absolute deviations method, linear programmingReferences
- Balunov K.A., Solyaev Yu.O., Golubkin K.S. Trudy MAI: elektron. zhurn., 2023, no. 129, 30 p. DOI 10.34759/trd-2023-129-04.
- Kornev S.V., Pimenov I.A. Trudy MAI: elektron. zhurn., 2022, no. 123, 23 p. DOI 10.34759/trd-2022-123-07.
- Stepanov R.P., Kusyumov A.N., Mikhaylov S.A., Tarasov N.N. Trudy MAI: elektron. zhurn., 2019, no. 107, 31 p. Avialable at: https://trudymai.ru/published.php?ID=107894.
- Abramova K.A., Sudakov V.G. Trudy MAI: elektron. zhurn., 2019, no. 105, 21 p. URL: https://trudymai.ru/published.php?ID=104133.
- Dababneh O., Conway-Smith J.T. An evaluation of the accuracy of existing empirical and semi-empirical methods for predicting the wing mass of large transport aircraft. Aerospace, 2025, vol. 12, no. 2, art. 142. DOI 10.3390/aerospace12020142.
- Wensheng Z.H.U., Zhouwei F.A.N., Xiongqing Y.U. Structural mass prediction in conceptual design of blended-wing-body aircraft. Chinese Journal of Aeronautics, 2019, vol. 32, no. 11, pp. 2455–2465. DOI 10.1016/j.cja.2019.08.003
- Resulkulyeva G., Serebryanskii S.A. Upravlenie razvitiem krupnomasshtabnykh sistem (MLSD'2022) : trudy pyatnadtsatoi mezhdunarodnoi konferentsii (26–28 sentyabrya 2022 g., Moskva, Rossiya) [Management of large-scale system development (MLSD'2022)], Moscow, IPU RAN, 2022. pp. 918–924.
- Espinosa Barcenas O.U., Lukyanov O.E. Izvestia of Samara Scientific Center of the Russian Academy of Sciences, 2020, vol. 22, no. 5, pp. 120–127. DOI 10.37313/1990-5378-2020-22-5-120-127.
- Dababneh O., Kipouros T. Aerospace Science and Technology, 2018, vol. 72, pp. 256–266. DOI 10.1016/j.ast.2017.11.006.
- Komarov V.A. Polet: obshcheros. nauch.-tekhn. Zhurnal, 2000, no. 1, pp. 31–39.
- Lapteva M.Yu. Izvestia of Samara Scientific Center of the Russian Academy of Sciences, 2011, vol. 13, no. 1/2, pp. 322–325.
- Sheynin V.M., Kozlovskiy V.I. Vesovoe proektirovanie i effektivnost' passazhirskikh samoletov [Weight design and efficiency of passenger aircraft]. Moscow, Mashinostroenie Publ., 1984. 552 p.
- Eger S.M., Mishin V.F., Liseytsev N.K. et al. Proektirovanie samoletov [Aircraft design]. Moscow, Logos, 2005. 648 p.
- Yarygina M.V. Design and weight analysis of a folding wing structure. Trudy MAI: elektron. zhurn., 2012, no. 51, 24 p. Avialable at: https://trudymai.ru/upload/iblock/f98/proektirovanie-i-vesovoy-analiz-konstruktsii-skladnogo-kryla.p....
- Litvinov V.M., Litvinov E.V. Metody rascheta massy konstruktsii letatel'nogo apparata po trebovaniyam prochnosti i zhestkosti [Methods for calculating the mass of an aircraft structure based on strength and rigidity requirements]. Moscow, TsAGI Publ., 2008, 202 p.
- Vyshinsky L.L., Flerov Yu.A. Informatics and Applications, 2021, vol. 15, no. 4, P. 93–102. DOI 10.14357/19922264210413.
- Caner M. A note on least absolute deviation estimation of a threshold model. Econometric Theory. 2002. vol. 18, no. 3, pp. 800–814. DOI 10.1017/S0266466602183113.
- Demidenko E.Z. Lineinaya i nelineinaya regressii [Linear and non-linear regressions]. Moscow, Finance & Statistics Publ., 1981, 303 p.
- Bazilevskiy M.P. International Journal of Open Information Technologies, 2024, vol. 12, no. 6, pp. 76–81.
- Bazilevskiy M.P. Digital Models and Solutions, 2024, vol. 3, no. 4, pp. 79–90. DOI 10.29141/2949-477X-2024-3-4-5.
- Patachakov I.V., Boos I.Yu., Gushcha D.I., Eretnov N.V., Aktelova A.Yu. Mine Surveying Bulletin, 2019, no. 6, pp. 53–57.
- Mohajan H.K. Estimation of cost minimization of garments sector by Cobb-Douglas production function: Bangladesh perspective. Annals of Spiru Haret University. Economic Series, 2021, vol. 21, no. 2, pp. 267–299.
- Bazilevskiy M.P. Applied Mathematics and Control Sciences, 2020, no. 2, pp. 41 54.
- Bazilevskiy M.P. Applied Mathematics and Control Sciences, 2023, no. 1, pp. 102 115.
Download

