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Synthesis of control laws for aircraft lateral motion at the lack of data on the slip angle: Analytical solution

  • Flight Dynamics and Control of Flight Vehicles
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Abstract

The problem of lateral motion stabilization is analytically solved for the fourth-order model of aircraft motion using the method of output signal control synthesis that is based on the control object decomposition. Numerical simulation data are presented.

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References

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Authors and Affiliations

  1. Bauman Moscow State Technical University, ul. Vtoraya Baumanskaya 5, Moscow, 105005, Russia

    N. E. Zubov, E. A. Mikrin, V. N. Ryabchenko & A. V. Fomichev

Authors
  1. N. E. Zubov
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  2. E. A. Mikrin
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  3. V. N. Ryabchenko
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  4. A. V. Fomichev
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Corresponding author

Correspondence to N. E. Zubov.

Additional information

Original Russian Text © N.E. Zubov, E.A. Mikrin, V.N. Ryabchenko, A.V. Fomichev, 2017, published in Izvestiya Vysshikh Uchebnykh Zavedenii, Aviatsionnaya Tekhnika, 2017, No. 1, pp. 61–70.

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Zubov, N.E., Mikrin, E.A., Ryabchenko, V.N. et al. Synthesis of control laws for aircraft lateral motion at the lack of data on the slip angle: Analytical solution. Russ. Aeronaut. 60, 64–73 (2017). https://doi.org/10.3103/S106879981701010X

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  • DOI: https://doi.org/10.3103/S106879981701010X

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