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Algorithm for identifying parameters of the dynamic system of an aircraft. II

  • Control Systems of Moving Objects
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Journal of Computer and Systems Sciences International Aims and scope

Abstract

The problem of identification of aerodynamic parameters of IL-96-300 aircraft by processing digital information on its longitudinal and lateral motion provided by on-board measurement complex according to real flight data (longitudinal motion) and results of mathematical simulation (lateral motion) is studied. The problem of algorithmic parameter identification for the nonlinear dynamic system, whose model corresponds to the control system of a modern maneuvering aircraft, is considered.

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References

  1. I. A. Boguslavskii, O. V. Kruglyakova, N. Ya. Miroshichev, and G. M. Tsimbalyuk, “Algorithm for Identifying Parameters of the Dynamic System of an Aircraft”, Izv. Ross. Akad. Nauk, Teor. Sist. Upr., No. 3 (2009) [Comp. Syst. Sci. 48 (4), 333–344 (2009)].

  2. S. V. Konstantinov, P. G. Red’ko, and S. A. Ermakov, Electrohydraulic Steering Drives of Maneuvering Aircraft Flight Control Systems (Yanus-K, Moscow, 2006) [in Russian].

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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, 2010, published in Izvestiya Akademii Nauk. Teoriya i Sistemy Upravleniya, 2010, No. 4, pp. 108–116.

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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. II. J. Comput. Syst. Sci. Int. 49, 615–623 (2010). https://doi.org/10.1134/S106423071004012X

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  • DOI: https://doi.org/10.1134/S106423071004012X

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