DE69614532D1 - Eigenfrequenznachlaufanordnung für faseroptische sensorspule - Google Patents

Eigenfrequenznachlaufanordnung für faseroptische sensorspule

Info

Publication number
DE69614532D1
DE69614532D1 DE69614532T DE69614532T DE69614532D1 DE 69614532 D1 DE69614532 D1 DE 69614532D1 DE 69614532 T DE69614532 T DE 69614532T DE 69614532 T DE69614532 T DE 69614532T DE 69614532 D1 DE69614532 D1 DE 69614532D1
Authority
DE
Germany
Prior art keywords
optical sensor
natural frequency
fiber optical
sensor coil
frequency tracking
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.)
Expired - Lifetime
Application number
DE69614532T
Other languages
English (en)
Other versions
DE69614532T2 (de
Inventor
K Strandjord
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.)
Honeywell Inc
Original Assignee
Honeywell Inc
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 Honeywell Inc filed Critical Honeywell Inc
Application granted granted Critical
Publication of DE69614532D1 publication Critical patent/DE69614532D1/de
Publication of DE69614532T2 publication Critical patent/DE69614532T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime 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
    • G01C19/72Gyrometers 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
DE69614532T 1995-06-07 1996-06-07 Eigenfrequenznachlaufanordnung für faseroptische sensorspule Expired - Lifetime DE69614532T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US47692095A 1995-06-07 1995-06-07
PCT/US1996/010125 WO1996041132A1 (en) 1995-06-07 1996-06-07 Proper frequency tracker for fiber optic sensing coil

Publications (2)

Publication Number Publication Date
DE69614532D1 true DE69614532D1 (de) 2001-09-20
DE69614532T2 DE69614532T2 (de) 2002-05-23

Family

ID=23893794

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69614532T Expired - Lifetime DE69614532T2 (de) 1995-06-07 1996-06-07 Eigenfrequenznachlaufanordnung für faseroptische sensorspule

Country Status (6)

Country Link
US (1) US5734469A (de)
EP (1) EP0830570B1 (de)
JP (1) JP3990450B2 (de)
CA (1) CA2221261A1 (de)
DE (1) DE69614532T2 (de)
WO (1) WO1996041132A1 (de)

Families Citing this family (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6629255B1 (en) * 2000-05-22 2003-09-30 Intel Corporation Generating a 2-phase clock using a non-50% divider circuit
US6798523B2 (en) 2001-12-04 2004-09-28 Honeywell International Inc. Sensor and method for detecting fiber optic faults
US6765678B2 (en) * 2002-01-08 2004-07-20 Honeywell International Inc. Relative intensity noise controller with maximum gain at frequencies at or above the bias modulation frequency or with second order feedback for fiber light sources
US6778279B2 (en) * 2002-02-19 2004-08-17 Honeywell International, Inc. Inline sagnac fiber optic sensor with modulation adjustment
US7038783B2 (en) * 2003-05-23 2006-05-02 Honeywell International Inc. Eigen frequency detector for Sagnac interferometers
KR100606100B1 (ko) * 2004-01-15 2006-07-28 삼성전자주식회사 바이어스 제어장치를 구비한 광변조장치 및 이를 이용한바이어스 제어방법
JP2006173213A (ja) * 2004-12-13 2006-06-29 Advantest Corp 温度安定化装置及び発振装置
US7333209B2 (en) * 2005-11-09 2008-02-19 Honeywell International, Inc. Fiber optic gyroscope asynchronous demodulation
US7872758B2 (en) * 2007-01-22 2011-01-18 The Charles Stark Draper Laboratory, Inc. Determining and compensating for modulator dynamics in interferometric fiber-optic gyroscopes
US7817284B2 (en) * 2007-08-08 2010-10-19 The Charles Stark Draper Laboratory, Inc. Interferometric fiber optic gyroscope with off-frequency modulation signals
US8027590B2 (en) * 2008-09-19 2011-09-27 Goodrich Corporation System and method for signal extraction by path modulation
US8223341B2 (en) 2010-05-28 2012-07-17 Honeywell International Inc. System and method for enhancing signal-to-noise ratio of a resonator fiber optic gyroscope
US8213019B2 (en) 2010-09-07 2012-07-03 Honeywell International Inc. RFOG with optical heterodyning for optical signal discrimination
US8717575B2 (en) 2011-08-17 2014-05-06 Honeywell International Inc. Systems and methods for environmentally insensitive high-performance fiber-optic gyroscopes
US8908187B2 (en) 2011-11-02 2014-12-09 Honeywell International Inc. System and method for reducing errors in a resonator fiber optic gyroscope
FR2983574B1 (fr) * 2011-12-06 2014-01-10 Sagem Defense Securite Capteur angulaire inertiel de type mems equilibre et procede d'equilibrage d'un tel capteur
US8830479B2 (en) 2013-01-28 2014-09-09 Honeywell International Inc. RFOG with optical heterodyning for optical signal discrimination
US8947671B2 (en) 2013-02-22 2015-02-03 Honeywell International Inc. Method and system for detecting optical ring resonator resonance frequencies and free spectral range to reduce the number of lasers in a resonator fiber optic gyroscope
US9001336B1 (en) 2013-10-07 2015-04-07 Honeywell International Inc. Methods and apparatus of tracking/locking resonator free spectral range and its application in resonator fiber optic gyroscope
CN104296740B (zh) * 2014-09-26 2017-05-31 北京控制工程研究所 一种基于反熔丝fpga的光纤陀螺主控板晶振选取方法
US10767995B2 (en) 2018-08-28 2020-09-08 Honeywell International Inc. Hyperbolic modulation offset error reducer for an RFOG
RU2764704C1 (ru) * 2020-10-28 2022-01-19 Александр Александрович Скрипкин Волоконно-оптический гироскоп

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB8611394D0 (en) * 1986-05-08 1986-10-29 British Aerospace Fibre optic gyroscopes
US4883358A (en) * 1987-09-02 1989-11-28 Japan Aviation Electronics Industry Limited Fiber optic gyro stabilized by harmonic components of detected signal
US5131750A (en) * 1990-06-04 1992-07-21 Honeywell Inc. Eigenfrequency phase shift control loop
US5090809A (en) * 1990-06-04 1992-02-25 Ferrar Carl M Modulation frequency control in a fiber optic rotation sensor
US5285257A (en) * 1991-03-01 1994-02-08 Matsushita Electric Industrial Co., Ltd. Optic rotation sensing apparatus and related method including providing synchronous detection at a phase at which the AM noise is minimized
FR2679647B1 (fr) * 1991-07-25 1993-11-05 Applications Gles Elect Meca Gyrometre interferometrique a modulateur electro-optique.

Also Published As

Publication number Publication date
JP3990450B2 (ja) 2007-10-10
CA2221261A1 (en) 1996-12-19
DE69614532T2 (de) 2002-05-23
WO1996041132A1 (en) 1996-12-19
EP0830570A1 (de) 1998-03-25
JPH11511246A (ja) 1999-09-28
US5734469A (en) 1998-03-31
EP0830570B1 (de) 2001-08-16

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