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Modeling the Motion of an Aircraft during Vertical Landing in Crosswind Conditions

  • FLIGHT DYNAMICS AND CONTROL OF FLIGHT VEHICLES
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Abstract

The paper considers the problem of increasing the safety of landing for small unmanned aerial vehicles under unfavorable external conditions, in particular, in the presence of gusty crosswind. A mathematical model describing the landing of a small unmanned aerial vehicle in the presence of aerodynamic flows and the stabilization in the XY plane is presented.

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ACKNOWLEDGEMENTS

This study was supported by the Ministry of Science and Higher Education of the Russian Federation in the framework of the Agreement no. 14.577.21.0284 of June 18, 2019 (unique project identifier is RFMEFI57717X0284).

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Authors and Affiliations

  1. Derzhavin Tambov State University, ul. Internatsional’naya 33, 392000, Tambov, Russia

    M. F. Gasanov, I. I. Pasechnikov & A. V. Krayukhin

  2. Baltic State Technical University “VOENMEH”, ul. 1ya Krasnoarmeiskaya 1, 190005, St. Petersburg, Russia

    A. I. Mel’nikova

Authors
  1. M. F. Gasanov
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  2. I. I. Pasechnikov
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  3. A. V. Krayukhin
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  4. A. I. Mel’nikova
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Corresponding author

Correspondence to M. F. Gasanov.

Additional information

Translated from Izvestiya Vysshikh Uchebnykh Zavedenii, Aviatsionnaya Tekhnika, 2020, No. 4, pp. 192 - 196.

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Gasanov, M.F., Pasechnikov, I.I., Krayukhin, A.V. et al. Modeling the Motion of an Aircraft during Vertical Landing in Crosswind Conditions. Russ. Aeronaut. 63, 771–775 (2020). https://doi.org/10.3103/S1068799820040273

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  • DOI: https://doi.org/10.3103/S1068799820040273

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