FR2592478A1 - Gyroscope a laser en anneau compense en puissance optique. - Google Patents

Gyroscope a laser en anneau compense en puissance optique.

Info

Publication number
FR2592478A1
FR2592478A1 FR8519254A FR8519254A FR2592478A1 FR 2592478 A1 FR2592478 A1 FR 2592478A1 FR 8519254 A FR8519254 A FR 8519254A FR 8519254 A FR8519254 A FR 8519254A FR 2592478 A1 FR2592478 A1 FR 2592478A1
Authority
FR
France
Prior art keywords
frequency
optical power
dihedral
laser gyroscope
waves
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
FR8519254A
Other languages
English (en)
Other versions
FR2592478B1 (fr
Inventor
William H Nelson
Albert N Zampiello
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 FR2592478A1 publication Critical patent/FR2592478A1/fr
Application granted granted Critical
Publication of FR2592478B1 publication Critical patent/FR2592478B1/fr
Anticipated expiration legal-status Critical
Expired - Fee Related 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

Landscapes

  • Physics & Mathematics (AREA)
  • Optics & Photonics (AREA)
  • Engineering & Computer Science (AREA)
  • Electromagnetism (AREA)
  • Power Engineering (AREA)
  • General Physics & Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Gyroscopes (AREA)
  • Lasers (AREA)

Abstract

L'invention consiste en un gyroscope à laser en anneau avec une compensation du signal de sortie pour les variations de puissance optique en fonction d'une fréquence dièdre. Le gyroscope comporte une cavité 20 avec un trajet fermé 30 et un agent de gain 26. Des réflecteurs 32, 34, 36, 38 produisent un déphasage dépendant du sens des ondes en polarisation circulaire, conduisant à une séparation de fréquences entre les ondes de même sens de polarisation. Un détecteur 22, 23, 48 détecte la fréquence dièdre et un processeur commande le signal de sortie en fonction des variations de la fréquence dièdre. L'invention s'applique à des gyroscopes de navigation. (CF DESSIN DANS BOPI)
FR858519254A 1983-11-07 1985-12-26 Gyroscope a laser en anneau compense en puissance optique. Expired - Fee Related FR2592478B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/549,357 US4652132A (en) 1983-11-07 1983-11-07 Optical power compensated ring laser gyroscope

Publications (2)

Publication Number Publication Date
FR2592478A1 true FR2592478A1 (fr) 1987-07-03
FR2592478B1 FR2592478B1 (fr) 1991-06-07

Family

ID=24192684

Family Applications (1)

Application Number Title Priority Date Filing Date
FR858519254A Expired - Fee Related FR2592478B1 (fr) 1983-11-07 1985-12-26 Gyroscope a laser en anneau compense en puissance optique.

Country Status (4)

Country Link
US (1) US4652132A (fr)
JP (1) JPH0750804B2 (fr)
DE (1) DE3609729C2 (fr)
FR (1) FR2592478B1 (fr)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4836675A (en) * 1987-06-29 1989-06-06 Litton Systems, Inc. Apparatus and method for detecting rotation rate and direction of rotation and providing cavity length control in multioscillator ring laser gyroscopes
US4963026A (en) * 1988-03-14 1990-10-16 Litton Systems, Inc. Cavity length control apparatus for a multi-oscillator
GB2227879B (en) * 1989-02-03 1994-02-09 Ferranti Int Signal Multi-oscillator ring laser gyroscope
GB2227878B (en) * 1989-02-03 1992-04-22 Ferranti Int Signal Ring laser gyroscope
US5116132A (en) * 1990-01-12 1992-05-26 Litton Systems, Inc. Ring laser gyroscope output optics detection system
US5088824A (en) * 1990-07-31 1992-02-18 Honeywell Inc. Laser beam control for a ring-laser gyro
US5374990A (en) * 1991-01-11 1994-12-20 Litton Systems, Inc. Active magnetic field tuning for dispersion equalization of a multi-oscillator
US5283627A (en) * 1991-05-09 1994-02-01 Honeywell Inc. System for inhibiting quenching of laser beams in response to radiation events
US5751425A (en) * 1996-12-30 1998-05-12 Litton Systems, Inc. Apparatus and method for detecting rotation rate, Faraday bias and cavity length in a ring laser gyroscope
CN114915232B (zh) * 2022-05-10 2023-07-04 电子科技大学 基于Speedgoat的励磁同步电机控制系统

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3854819A (en) * 1971-03-03 1974-12-17 K Andringa Laser gyroscope
GB2087638A (en) * 1980-10-17 1982-05-26 Raytheon Co Ring laser gyroscope

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4110045A (en) * 1976-01-02 1978-08-29 Raytheon Company Electromagnetic wave ring resonator
US4108553A (en) * 1977-01-04 1978-08-22 Raytheon Company Laser gyroscope detector and path length control system
US4141651A (en) * 1977-01-10 1979-02-27 Raytheon Company Laser gyroscope output optics structure
CA1136249A (fr) * 1978-03-27 1982-11-23 James B. Matthews Systeme gyroscopique a laser a boucle a asservissement de phase
DE2821241C2 (de) * 1978-05-16 1984-04-19 Litton Systems, Inc., 90210 Beverly Hills, Calif. Ring-Laser-Gyroskop
US4213705A (en) * 1978-11-09 1980-07-22 Litton Systems, Inc. Four mode Zeeman laser gyroscope with minimum hole burning competition
JPS5628036A (en) * 1979-08-14 1981-03-19 Toyota Motor Corp Tandem brake oil-hydraulic controller having bypass means
US4470701A (en) * 1980-10-17 1984-09-11 Raytheon Company Dispersion equalized ring laser gyroscope
JPS5870167A (ja) * 1981-07-06 1983-04-26 ハネウエル・インコ−ポレ−テツド 角速度センサ
JPS5832793A (ja) * 1981-08-19 1983-02-25 株式会社マルサン ブロツク玩具
JPS5833719A (ja) * 1981-08-20 1983-02-28 Canon Inc 信号発生装置
JPS58100478A (ja) * 1981-12-10 1983-06-15 Japan Aviation Electronics Ind Ltd レ−ザジヤイロの読取装置
US4551021A (en) * 1982-03-01 1985-11-05 Honeywell Inc. Discriminant apparatus for laser gyros
US4526469A (en) * 1982-03-01 1985-07-02 Honeywell Inc. Discriminant apparatus for laser gyros

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3854819A (en) * 1971-03-03 1974-12-17 K Andringa Laser gyroscope
GB2087638A (en) * 1980-10-17 1982-05-26 Raytheon Co Ring laser gyroscope

Also Published As

Publication number Publication date
JPS62166579A (ja) 1987-07-23
DE3609729A1 (de) 1987-09-24
FR2592478B1 (fr) 1991-06-07
US4652132A (en) 1987-03-24
DE3609729C2 (de) 1997-04-03
JPH0750804B2 (ja) 1995-05-31

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Legal Events

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ST Notification of lapse