GB2017392A - Phase-locked loop laser gyroscope - Google Patents

Phase-locked loop laser gyroscope

Info

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
Application number
GB7908589A
Other versions
GB2017392B (en
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Raytheon Co
Original Assignee
Raytheon Co
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Raytheon Co filed Critical Raytheon Co
Publication of GB2017392A publication Critical patent/GB2017392A/en
Application granted granted Critical
Publication of GB2017392B publication Critical patent/GB2017392B/en
Expired legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01CMEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C19/00Gyroscopes; Turn-sensitive devices using vibrating masses; Turn-sensitive devices without moving masses; Measuring angular rate using gyroscopic effects
    • G01C19/58Turn-sensitive devices without moving masses
    • G01C19/64Gyrometers using the Sagnac effect, i.e. rotation-induced shifts between counter-rotating electromagnetic beams
    • G01C19/66Ring laser gyrometers
    • G01C19/667Ring 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>
GB7908589A 1978-03-27 1979-03-12 Phase-locked loop laser gyroscope Expired GB2017392B (en)

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)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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

Cited By (11)

* Cited by examiner, † Cited by third party
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