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Synthesis of Stabilization Laws for Lateral Motion of a Maneuverable Aircraft at the Lack of Data on Its Sideslip and Roll Angles

  • Flight Dynamics and Control of Flight Vehicles
  • Published:
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Abstract

The problem of synthesizing stabilization laws for lateral motion of a maneuverable aircraft at the lack of data on its sideslip and roll angles is analytically solved. The solution is based on the improved method of output signal control synthesis, which provides the specified spectrum of MIMO-system motion. The results of analytical synthesis of the control law and numerical simulation data are presented.

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Acknowledgements

The work is supported by the Russian Science Foundation, project no. 19-19-00031.

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Authors and Affiliations

  1. Bauman Moscow State Technical University, ul. 2-ya Baumanskaya 5, Moscow, 105005, Russia

    N. E. Zubov & V. N. Ryabchenko

  2. Korolev Rocket and Space Corporation Energiya, ul. Lenina 4a, Korolev, Moscow region, 141070, Russia

    E. A. Mikrin & I. V. Sorokin

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. I. V. Sorokin
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Correspondence to N. E. Zubov.

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Zubov, N.E., Mikrin, E.A., Ryabchenko, V.N. et al. Synthesis of Stabilization Laws for Lateral Motion of a Maneuverable Aircraft at the Lack of Data on Its Sideslip and Roll Angles. Russ. Aeronaut. 62, 22–31 (2019). https://doi.org/10.3103/S1068799819010045

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  • DOI: https://doi.org/10.3103/S1068799819010045

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