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Wave Solid-State Gyroscopes of Russian Design for Aircraft Onboard Systems

Russian Aeronautics volume 64, pages 749–755 (2021)Cite this article

Abstract

This paper considers wave solid-state gyroscopes with volumetric resonators operating in the mode of angular velocity sensors for onboard control systems and flight safety. The results of laboratory bench tests of wave solid-state gyroscopes with metal cylindrical and silicon ring resonators are presented. Possibilities of their use in aircraft onboard systems are indicated.

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ACKNOWLEDGEMENTS

The work was supported by the grant of the Government of the Tula region in the field of science and technology, no. DS1264, of October 25, 2021.

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Authors and Affiliations

  1. Tula State University, pr. Lenina 92, 300012, Tula, Russia

    V. Ya. Raspopov, V. V. Likhosherst & A. V. Kalikanov

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  1. V. Ya. Raspopov
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  2. V. V. Likhosherst
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  3. A. V. Kalikanov
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Correspondence to V. Ya. Raspopov.

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Raspopov, V.Y., Likhosherst, V.V. & Kalikanov, A.V. Wave Solid-State Gyroscopes of Russian Design for Aircraft Onboard Systems. Russ. Aeronaut. 64, 749–755 (2021). https://doi.org/10.3103/S1068799821040218

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  • DOI: https://doi.org/10.3103/S1068799821040218

Keywords

  • aircraft
  • onboard system
  • wave solid-state gyroscope
  • resonators
  • tests