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Computationally effective mathematical model of airplane flight

  • Flight Dynamics and Control of Flight Vehicles
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Abstract

An approach to modeling is proposed, where the airplane is considered as a system with a minimal set of basic material points, and its mathematical description is given. We construct the mathematical model of the conventional airplane with an adequate accuracy for evaluation calculations in creating the control system. The flight simulation software for the Yak-52 and NG-4 airplanes is developed in MATLAB and the modeling results are analyzed.

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References

  1. Galashev, E.S., Lysenko, N.M., Mikoyan, S.A., Nekrasov, V.I., Nechaev, Yu.N., Nisht, M.I., Radchenko, M.I., and Sivkov, G.F., Aerodinamika i dinamika poleta manevrennykh samoletov (Aerodynamics and Flight Dynamics of Maneuverable Aircraft), Moscow: Voenizdat, 1984.

    Google Scholar 

  2. Balakin, V.L. and Lazarev Yu.N., Dinamika poleta samoleta. Ustoichivost’ i upravlyaemost’ prodol’nogo dvizheniya (Flight Dynamics of the Aircraft. Longitudinal Movement Stability and Control), Samara: SSAU, 2011.

    Google Scholar 

  3. Eger, S.M., Proektirovanie samoletov (Aircraft Design), Moscow: Mashinostroenie, 1983.

    Google Scholar 

  4. Bekhtina, N.B. and Kublanov, M.S., Dinamika poleta. Posobie po vypolneniyu laboratornykh rabot na PEVM (Flight Dynamics. Guide for the Implementation of Laboratory Works on PC), Moscow: MGTU GA, 2007.

    Google Scholar 

  5. Garkushenko, V.I. and Lazareva, P.A., To a Problem of Aircraft Control System Design with Given Dynamic Parameters, Izv. Vuz. Av. Tekhnika, 2015, vol. 58, no. 4, pp. 15–20 [Russian Aeronautics (Engl.Transl.), vol. 58, no. 4, pp. 383–387].

    Google Scholar 

  6. Chasovnikov, E.A., On the Issue of Dividing the Aerodynamic Derivative Systems for the Aircraft Flight Dynamics Problems, Izv. Vuz. Av. Tekhnika, 2011, vol. 54, no. 3, pp. 47–49 [Russian Aeronautics (Engl.Transl.), vol. 54, no. 3, pp. 298–302].

    Google Scholar 

  7. Gainutdinov, V.G., An Algorithm for Computer-Aided Design Calculation of Aircraft Stability and Controllability Parameters, Izv. Vuz. Av. Tekhnika, 2010, vol. 53, no. 3, pp. 24–27 [Russian Aeronautics (Engl.Transl.), vol. 53, no. 3, pp. 277–282].

    Google Scholar 

  8. Syzdykov, E.K. and Gainutdinova, A.V., Design Calculation of Light Piston-Engined Aircraft Controllability and Stability Parameters, Izv. Vuz. Av. Tekhnika, 2010, vol. 53, no. 2, pp. 12–15 [Russian Aeronautics (Engl.Transl.), vol. 53, no. 2, pp. 134–140].

    Google Scholar 

  9. Korovin, A.E. and Novikov, Yu.F., Prakticheskaya aerodinamika i dinamika poleta samoletov YaK-52 i YaK-55 (Practical Aerodynamics and Flight Dynamics of the Yak-52 and Yak-55 Aircraft), Moscow: DOSAAF, 1989.

    Google Scholar 

  10. The NG-4UL Airplane Flight Manual, ROKO AERO A.S., 2008.

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Correspondence to D. Yu. Kudryavtsev.

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Original Russian Text © D.Yu. Kudryavtsev, D.A. Aminev, A.S. Sviridov, 2016, published in Izvestiya Vysshikh Uchebnykh Zavedenii, Aviatsionnaya Tekhnika, 2016, No. 3, pp. 45–51.

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Kudryavtsev, D.Y., Aminev, D.A. & Sviridov, A.S. Computationally effective mathematical model of airplane flight. Russ. Aeronaut. 59, 344–350 (2016). https://doi.org/10.3103/S1068799816030089

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  • DOI: https://doi.org/10.3103/S1068799816030089

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