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Design of unmanned aerial vehicle structure and stabilization system for aeroelastic stability

  • Flight Dynamics and Control of Flight Vehicles
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Abstract

An approach is proposed to solving the problem of collaborative design of the structure and stabilization system of a maneuverable unmanned aerial vehicle (UAV) taking into account the requirements of aeroelastic stability. The models and methods, which employ this approach, are described.

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Authors and Affiliations

  1. Moscow Aviation Institute, National Research University, Volokolamskoe shosse 4, Moscow, 125993, Russia

    S. G. Parafes’

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  1. S. G. Parafes’
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Correspondence to S. G. Parafes’.

Additional information

Original Russian Text © S.G. Parafes’, 2015, published in Izvestiya VUZ. Aviatsionnaya Tekhnika, 2015, No. 3, pp. 21–27.

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Parafes’, S.G. Design of unmanned aerial vehicle structure and stabilization system for aeroelastic stability. Russ. Aeronaut. 58, 271–278 (2015). https://doi.org/10.3103/S1068799815030046

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  • DOI: https://doi.org/10.3103/S1068799815030046

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