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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Veröffentlicht in:	Cosmic research 2009-02, Vol.47 (1), p.68-74
Hauptverfasser:	Voiskovskii, M. I., Gorshkov, A. N., Evlanov, E. N., Zubkov, B. V., Podkolzin, S. N., Linkin, V. M.
Format:	Artikel
Sprache:	eng
Schlagworte:	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
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Beschreibung
Zusammenfassung:	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.
ISSN:	0010-9525 1608-3075
DOI:	10.1134/S0010952509010080