GB2017392A - Phase-locked loop laser gyroscope - Google Patents
Phase-locked loop laser gyroscopeInfo
- Publication number
- GB2017392A GB2017392A GB7908589A GB7908589A GB2017392A GB 2017392 A GB2017392 A GB 2017392A GB 7908589 A GB7908589 A GB 7908589A GB 7908589 A GB7908589 A GB 7908589A GB 2017392 A GB2017392 A GB 2017392A
- Authority
- GB
- United Kingdom
- Prior art keywords
- frequency
- delta
- phase
- difference
- locked
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
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
- G01C19/66—Ring laser gyrometers
- G01C19/667—Ring laser gyrometers using a multioscillator ring laser
Abstract
A laser gyroscope has a phased-locked loop circuit 5, Fig. 1, coupled to a frequency difference output from a laser gyroscope cavity 110. Waves of four frequencies propagate around the gyroscope cavity, each characterised by one of the two different senses of circular polarization and one of the two different directions of propagation. Output signals DELTA f1 and DELTA f2 are formed each having a frequency equal to the difference between the frequencies of a corresponding wave pair. The frequency difference signal DELTA f1 for one wave pair is phase-locked to an external reference source 118, Fig. 3. A signal applied to a Faraday rotator bias coil 114 provides the frequency shifting of the wave pairs necessary to achieve a constant frequency difference DELTA f1. The amplitude of the signal applied to the Faraday bias coil can be employed as a precise measure Vout of the rate of rotation. Alternatively, a second, external phase-locked loop, Fig. 4, includes a voltage controlled oscillator 138 followed by a frequency divider 135 whereby the oscillator frequency divided by N is phase locked to DELTA f2. The output of the voltage controlled oscillator provides an output signal Vout which has a frequency in proportion to but many times higher than the frequencies of the wave pair difference signals. in a further alternative not controlling the frequency difference in the laser, the control signal for the voltage controlled oscillator 138 provides the measure of rate of rotation. Other embodiments employ phase- locked loops only of the external type. <IMAGE>
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US89042378A | 1978-03-27 | 1978-03-27 |
Publications (2)
Publication Number | Publication Date |
---|---|
GB2017392A true GB2017392A (en) | 1979-10-03 |
GB2017392B GB2017392B (en) | 1982-05-26 |
Family
ID=25396657
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB7908589A Expired GB2017392B (en) | 1978-03-27 | 1979-03-12 | Phase-locked loop laser gyroscope |
Country Status (4)
Country | Link |
---|---|
JP (1) | JPS54139392A (en) |
CA (1) | CA1136249A (en) |
DE (1) | DE2911789A1 (en) |
GB (1) | GB2017392B (en) |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2118768A (en) * | 1982-04-21 | 1983-11-02 | Chevron Res | Frequency shifted cavity for electromagnetic radiation |
US4586184A (en) * | 1983-10-21 | 1986-04-29 | Chevron Research Company | Acoustically controlled frequency shifted cavity for electromagnetic radiation |
GB2184285A (en) * | 1983-11-07 | 1987-06-17 | Raytheon Co | Ring laser gyroscope |
EP1020706A1 (en) * | 1999-01-18 | 2000-07-19 | Canon Kabushiki Kaisha | Laser apparatus and gyroscope |
US6654126B1 (en) | 1999-12-01 | 2003-11-25 | Canon Kabushiki Kaisha | Optical gyro with specific clock/calculation circuit |
US6665330B1 (en) | 1999-09-14 | 2003-12-16 | Canon Kabushiki Kaisha | Semiconductor device having a semiconductor ring laser with a circularly formed ridge optical waveguide |
GB2419735A (en) * | 2004-03-16 | 2006-05-03 | Thales Sa | Four-mode stabilized solid-state gyrolaser without blind region |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CA1132692A (en) * | 1978-04-07 | 1982-09-28 | James B. Matthews | Phase-locked laser gyroscope system |
US4652132A (en) * | 1983-11-07 | 1987-03-24 | Raytheon Company | Optical power compensated ring laser gyroscope |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3697181A (en) * | 1967-03-14 | 1972-10-10 | Sperry Rand Corp | Ring laser having amplitude and phase controlled crossed-beam anti-locking feedback |
US3741657A (en) * | 1971-03-03 | 1973-06-26 | Raytheon Co | Laser gyroscope |
US3807866A (en) * | 1972-04-21 | 1974-04-30 | Rockwell International Corp | Ring laser gyroscope having a constant output beat-frequency |
US3846025A (en) * | 1973-04-02 | 1974-11-05 | S Wilber | Frequency sensitive laser rotary motion sensor |
-
1979
- 1979-03-05 CA CA000322871A patent/CA1136249A/en not_active Expired
- 1979-03-12 GB GB7908589A patent/GB2017392B/en not_active Expired
- 1979-03-26 DE DE2911789A patent/DE2911789A1/en active Granted
- 1979-03-26 JP JP3540979A patent/JPS54139392A/en active Granted
Cited By (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2118768A (en) * | 1982-04-21 | 1983-11-02 | Chevron Res | Frequency shifted cavity for electromagnetic radiation |
US4697888A (en) * | 1982-04-21 | 1987-10-06 | Chevron Research Company | Frequency shifted cavity for electromagnetic radiation |
US4586184A (en) * | 1983-10-21 | 1986-04-29 | Chevron Research Company | Acoustically controlled frequency shifted cavity for electromagnetic radiation |
GB2184285A (en) * | 1983-11-07 | 1987-06-17 | Raytheon Co | Ring laser gyroscope |
GB2184285B (en) * | 1983-11-07 | 1990-08-01 | Raytheon Co | Ring laser gyroscope |
EP1020706A1 (en) * | 1999-01-18 | 2000-07-19 | Canon Kabushiki Kaisha | Laser apparatus and gyroscope |
US6741354B2 (en) | 1999-01-18 | 2004-05-25 | Canon Kabushiki Kaisha | Laser device having an optical waveguide for discerning movement of an optical gyroscope and an optical gyroscope utilizing same |
US6665330B1 (en) | 1999-09-14 | 2003-12-16 | Canon Kabushiki Kaisha | Semiconductor device having a semiconductor ring laser with a circularly formed ridge optical waveguide |
US6654126B1 (en) | 1999-12-01 | 2003-11-25 | Canon Kabushiki Kaisha | Optical gyro with specific clock/calculation circuit |
GB2419735A (en) * | 2004-03-16 | 2006-05-03 | Thales Sa | Four-mode stabilized solid-state gyrolaser without blind region |
GB2419735B (en) * | 2004-03-16 | 2007-12-05 | Thales Sa | Four-mode stabilized solid-state gyrolaser without blind region |
Also Published As
Publication number | Publication date |
---|---|
CA1136249A (en) | 1982-11-23 |
JPS54139392A (en) | 1979-10-29 |
JPS6141158B2 (en) | 1986-09-12 |
DE2911789A1 (en) | 1979-10-04 |
GB2017392B (en) | 1982-05-26 |
DE2911789C2 (en) | 1991-08-29 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PCNP | Patent ceased through non-payment of renewal fee |
Effective date: 19970312 |