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Three-axial fiber optic gyroscope

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Abstract

We consider a new design of a high-precision three-axial sensor of angular velocities whose sensitive elements are fiber optic gyroscopes using the Sagnac effect. The instrument is designed for measuring the rotation velocity of an orbiting spacecraft (microsatellite) and for performing its attitude control.

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References

  1. Alexander, Amir and Friedman, Luis D., Cosmos 1. The Journey Begins, Planetary report, 2004, vol. XXIV, no. 6.

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Authors and Affiliations

  1. Space Research Institute, Russian Academy of Sciences, ul. Profsoyuznaya 84/32, Moscow, 117810, Russia

    M. I. Voiskovskii, A. N. Gorshkov, E. N. Evlanov, B. V. Zubkov, S. N. Podkolzin & V. M. Linkin

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  1. M. I. Voiskovskii
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  2. A. N. Gorshkov
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  3. E. N. Evlanov
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  4. B. V. Zubkov
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  5. S. N. Podkolzin
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  6. V. M. Linkin
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Original Russian Text © M.I. Voiskovskii, A.N. Gorshkov, E.N. Evlanov, B.V. Zubkov, S.N. Podkolzin, V.M. Linkin 2009, published in Kosmicheskie Issledovaniya, 2009, Vol. 47, No. 1, pp. 85–91.

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Voiskovskii, M.I., Gorshkov, A.N., Evlanov, E.N. et al. Three-axial fiber optic gyroscope. Cosmic Res 47, 68–74 (2009). https://doi.org/10.1134/S0010952509010080

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  • DOI: https://doi.org/10.1134/S0010952509010080

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