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 |
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| container_end_page | 74 |
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| container_issue | 1 |
| container_start_page | 68 |
| container_title | Cosmic research |
| container_volume | 47 |
| creator | Voiskovskii, M. I. Gorshkov, A. N. Evlanov, E. N. Zubkov, B. V. Podkolzin, S. N. Linkin, V. M. |
| description | 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. |
| doi_str_mv | 10.1134/S0010952509010080 |
| format | Article |
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| ispartof | Cosmic research, 2009-02, Vol.47 (1), p.68-74 |
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| language | eng |
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| source | SpringerLink Journals |
| subjects | 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 |
| title | Three-axial fiber optic gyroscope |
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