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Algorithm for identifying parameters of the dynamic system of an aircraft

  • Data Processing and Identification
  • Published:
Journal of Computer and Systems Sciences International Aims and scope

Abstract

The parameter identification problem for the nonlinear dynamic system of a sufficiently general form, in which the multipolynomial approximation algorithm processes measured data, is considered. To show the efficiency of the algorithm, an example of parameter identification for a nonlinear dynamic system with non-differentiable right-hand side is given and the identification problem for aerodynamic parameters of aircraft pitching motion is solved.

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Authors and Affiliations

  1. State Scientific Research Institute for Aviation Systems, ul. Viktorenko 7, Moscow, 125319, Russia

    I. A. Boguslavskii, O. V. Kruglyakova, N. Ya. Miroshichev & G. M. Tsimbalyuk

  2. OAO Il’yushin Aviation Complex (OAO “IL”), Leningradskii prospect 45G, Moscow, 125190, Russia

    I. A. Boguslavskii, O. V. Kruglyakova, N. Ya. Miroshichev & G. M. Tsimbalyuk

Authors
  1. I. A. Boguslavskii
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  2. O. V. Kruglyakova
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  3. N. Ya. Miroshichev
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  4. G. M. Tsimbalyuk
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Additional information

Original Russian Text © I.A. Boguslavskii, O.V. Kruglyakova, N.Ya. Miroshichev, G.M. Tsimbalyuk, 2009, published in Izvestiya Akademii Nauk. Teoriya i Sistemy Upravleniya, 2009, No. 3, pp. 3–15.

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Boguslavskii, I.A., Kruglyakova, O.V., Miroshichev, N.Y. et al. Algorithm for identifying parameters of the dynamic system of an aircraft. J. Comput. Syst. Sci. Int. 48, 333–344 (2009). https://doi.org/10.1134/S1064230709030010

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  • DOI: https://doi.org/10.1134/S1064230709030010

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