SE7705329L - PROCEDURE AND DEVICE FOR SATURATION OF FAITH ROTATION - Google Patents
PROCEDURE AND DEVICE FOR SATURATION OF FAITH ROTATIONInfo
- Publication number
- SE7705329L SE7705329L SE7705329A SE7705329A SE7705329L SE 7705329 L SE7705329 L SE 7705329L SE 7705329 A SE7705329 A SE 7705329A SE 7705329 A SE7705329 A SE 7705329A SE 7705329 L SE7705329 L SE 7705329L
- Authority
- SE
- Sweden
- Prior art keywords
- beams
- passive ring
- countertravelling
- rotation
- inertial rotation
- Prior art date
Links
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C19/00—Gyroscopes; Turn-sensitive devices using vibrating masses; Turn-sensitive devices without moving masses; Measuring angular rate using gyroscopic effects
- G01C19/58—Turn-sensitive devices without moving masses
- G01C19/64—Gyrometers using the Sagnac effect, i.e. rotation-induced shifts between counter-rotating electromagnetic beams
- G01C19/72—Gyrometers using the Sagnac effect, i.e. rotation-induced shifts between counter-rotating electromagnetic beams with counter-rotating light beams in a passive ring, e.g. fibre laser gyrometers
- G01C19/727—Gyrometers using the Sagnac effect, i.e. rotation-induced shifts between counter-rotating electromagnetic beams with counter-rotating light beams in a passive ring, e.g. fibre laser gyrometers using a passive ring resonator
Landscapes
- Physics & Mathematics (AREA)
- Engineering & Computer Science (AREA)
- Optics & Photonics (AREA)
- Electromagnetism (AREA)
- Power Engineering (AREA)
- General Physics & Mathematics (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Lasers (AREA)
- Gyroscopes (AREA)
Abstract
A sensor for measuring inertial rotation is provided which includes a passive ring, a means for generating two beams of monochromatic electromagnetic radiation, means for passing the beams into the passive ring to form two countertravelling beams and means adapted to lock the beams entering the passive ring to the cavity resonant frequencies of the countertravelling beams. The amount and direction of inertial rotation is determined by determining the frequency of the beams entering the passive ring effected by the locking means and the frequency shift of the countertravelling beams resulting from the inertial rotation of the passive ring.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US05/683,982 US4135822A (en) | 1976-01-19 | 1976-05-06 | Laser gyroscope |
Publications (1)
Publication Number | Publication Date |
---|---|
SE7705329L true SE7705329L (en) | 1977-11-07 |
Family
ID=24746237
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SE7705329A SE7705329L (en) | 1976-05-06 | 1977-05-06 | PROCEDURE AND DEVICE FOR SATURATION OF FAITH ROTATION |
Country Status (5)
Country | Link |
---|---|
CA (1) | CA1072665A (en) |
DE (1) | DE2720256A1 (en) |
FR (1) | FR2350583A1 (en) |
GB (1) | GB1576941A (en) |
SE (1) | SE7705329L (en) |
Families Citing this family (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4208128A (en) * | 1978-08-23 | 1980-06-17 | Rockwell International Corporation | Interferometer gyro using heterodyne phase detection without severe light source coherence requirements |
CA1136744A (en) * | 1978-08-23 | 1982-11-30 | Rockwell International Corporation | Interferometer gyro using heterodyne phase detection |
US4299490A (en) * | 1978-12-07 | 1981-11-10 | Mcdonnell Douglas Corporation | Phase nulling optical gyro |
DE2934794A1 (en) * | 1979-08-29 | 1981-03-19 | Licentia Patent-Verwaltungs-Gmbh, 6000 Frankfurt | Absolute rotation speed measurement - using monochromatic light ring with single sideband modulation of opposed partial light beams |
DE3438184A1 (en) * | 1984-10-18 | 1986-04-24 | Bodenseewerk Gerätetechnik GmbH, 7770 Überlingen | Device for measuring rotational speeds |
US4661964A (en) * | 1985-10-02 | 1987-04-28 | Northrop Corporation | Resonant waveguide laser gyro with a switched source |
DE3928715C2 (en) * | 1989-08-30 | 1993-12-02 | Deutsche Aerospace | Fiber gyroscope |
DE4407348A1 (en) * | 1994-03-05 | 1995-09-07 | Bodenseewerk Geraetetech | Brillouin ring laser gyroscope |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3332314A (en) * | 1963-04-08 | 1967-07-25 | Kollsman Instr Corp | Optical interferometric navigational instrument |
US3373650A (en) * | 1965-04-02 | 1968-03-19 | Honeywell Inc | Laser angular rate sensor |
US3627422A (en) * | 1965-06-21 | 1971-12-14 | Varian Associates | Means for avoiding locking in ring lasers |
US3890047A (en) * | 1969-02-25 | 1975-06-17 | United Aircraft Corp | Differential laser gyro employing reflection polarization anisotropy |
FR2271542A1 (en) * | 1973-12-27 | 1975-12-12 | Minisini Pierre | Rotation measuring ring laser rate gyroscope - has two electro-optics crystals and two sensors for two laser beams |
US4013365A (en) * | 1974-08-29 | 1977-03-22 | The University Of Utah | Laser gyroscope |
-
1977
- 1977-05-05 DE DE19772720256 patent/DE2720256A1/en not_active Withdrawn
- 1977-05-05 FR FR7713785A patent/FR2350583A1/en active Granted
- 1977-05-06 GB GB1904277A patent/GB1576941A/en not_active Expired
- 1977-05-06 SE SE7705329A patent/SE7705329L/en not_active Application Discontinuation
- 1977-05-06 CA CA277,852A patent/CA1072665A/en not_active Expired
Also Published As
Publication number | Publication date |
---|---|
FR2350583B1 (en) | 1983-01-14 |
GB1576941A (en) | 1980-10-15 |
CA1072665A (en) | 1980-02-26 |
DE2720256A1 (en) | 1977-11-17 |
FR2350583A1 (en) | 1977-12-02 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
NAV | Patent application has lapsed |
Ref document number: 7705329-6 |