Three-axial fiber optic gyroscope

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...

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Vydané v:Cosmic research Ročník 47; číslo 1; s. 68 - 74
Hlavní autori: Voiskovskii, M. I., Gorshkov, A. N., Evlanov, E. N., Zubkov, B. V., Podkolzin, S. N., Linkin, V. M.
Médium: Journal Article
Jazyk:English
Vydavateľské údaje: Dordrecht SP MAIK Nauka/Interperiodica 01.02.2009
Springer Nature B.V
Predmet:
Angular velocity
Astronomy
Astrophysics and Astroparticles
Astrophysics and Cosmology
Attitude control
Fiber optic gyroscopes
Fiber optics
Measuring instruments
Microsatellites
Physics
Physics and Astronomy
Sagnac effect
Sensors
Space Exploration and Astronautics
Space Sciences (including Extraterrestrial Physics
Spacecraft
42.81.Pa
ISSN:0010-9525, 1608-3075
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Popis
Shrnutí: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.
Bibliografia:SourceType-Scholarly Journals-1
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ISSN:0010-9525
1608-3075
DOI:10.1134/S0010952509010080