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Modeling of helicopter behavior dynamics under the controlling action of the stabilization and control system

  • Structural Mechanics and Strength of Flight Vehicles
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Abstract

A possibility of evaluating dynamic response of a mechanical system to controlling actions of the automatic stabilization and control system is considered on the basis of a numerical experiment. Examples of design analysis are presented for a light-weight helicopter in which an autopilot is part of the control system. The finite element analysis is used in this paper.

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Authors and Affiliations

  1. Tupolev Kazan National Research Technical University, Kazan, Russia

    E. V. Kasumov

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  1. E. V. Kasumov
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Additional information

Original Russian Text © E.V. Kasumov, 2013, published in Izvestiya VUZ. Aviatsionnaya Tekhnika, 2013, No. 3, pp. 11–14.

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Kasumov, E.V. Modeling of helicopter behavior dynamics under the controlling action of the stabilization and control system. Russ. Aeronaut. 56, 224–228 (2013). https://doi.org/10.3103/S1068799813030033

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  • DOI: https://doi.org/10.3103/S1068799813030033

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