IL111820A0 - Modular laser gyro - Google Patents

Modular laser gyro

Info

Publication number
IL111820A0
IL111820A0 IL11182094A IL11182094A IL111820A0 IL 111820 A0 IL111820 A0 IL 111820A0 IL 11182094 A IL11182094 A IL 11182094A IL 11182094 A IL11182094 A IL 11182094A IL 111820 A0 IL111820 A0 IL 111820A0
Authority
IL
Israel
Prior art keywords
laser gyro
modular laser
modular
gyro
laser
Prior art date
Application number
IL11182094A
Other languages
English (en)
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
Publication of IL111820A0 publication Critical patent/IL111820A0/xx

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
    • G01C19/661Ring laser gyrometers details
    • 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

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)
  • Gyroscopes (AREA)
  • Lasers (AREA)
IL11182094A 1993-11-29 1994-11-29 Modular laser gyro IL111820A0 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US16155593A 1993-11-29 1993-11-29

Publications (1)

Publication Number Publication Date
IL111820A0 true IL111820A0 (en) 1995-01-24

Family

ID=22581668

Family Applications (1)

Application Number Title Priority Date Filing Date
IL11182094A IL111820A0 (en) 1993-11-29 1994-11-29 Modular laser gyro

Country Status (11)

Country Link
US (1) US6208414B1 (zh)
EP (1) EP0733196A1 (zh)
JP (1) JPH09505668A (zh)
KR (1) KR960706629A (zh)
CN (1) CN1145664A (zh)
AU (1) AU699978B2 (zh)
BR (1) BR9408186A (zh)
CA (1) CA2176752A1 (zh)
IL (1) IL111820A0 (zh)
NO (1) NO962183L (zh)
WO (1) WO1995014906A2 (zh)

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US5818591A (en) * 1997-11-26 1998-10-06 Honeywell Inc. Tailoring the RLG mirror lifetime by changing the mirror to plasma distance spacing
US20010049618A1 (en) * 2000-03-23 2001-12-06 Rainer Patzel Method for allocating predictable costs for consumable items
US6476918B1 (en) * 2001-06-21 2002-11-05 Honeywell International Inc. Dither control system for a ring laser gyro
US6683692B2 (en) * 2001-06-21 2004-01-27 Honeywell International Dither system for motion sensors
US6876926B2 (en) * 2002-09-26 2005-04-05 Honeywell International Inc. Method and system for processing pulse signals within an inertial navigation system
US7088452B2 (en) 2003-04-11 2006-08-08 Honeywell International Inc. Dither stripper with non-linearity correction
US20060028260A1 (en) * 2004-08-04 2006-02-09 Baumgartner Richard A Logarithmic amplifier with base and emitter in feedback path
US7382463B2 (en) * 2005-01-28 2008-06-03 Honeywell International Inc. Methods and systems for improving optical flatness in a path length control driver
US7289924B2 (en) * 2005-07-20 2007-10-30 Honeywell International Inc. Self-calibrating sensor
US7375816B2 (en) * 2005-09-29 2008-05-20 Honeywell International Inc. Dither motor having integrated drive and pickoff transducers
US7440109B1 (en) 2006-06-28 2008-10-21 The United States Of America As Represented By The Secretary Of The Navy Dither stripper having least-mean-squares adaptive updating of dither stripper gains
US7633626B2 (en) * 2006-12-13 2009-12-15 Northrop Grumman Guidance and Electronics Co., Inc. Fiber optic gyroscope deadband circumvention apparatus and method
US20100077856A1 (en) * 2008-02-15 2010-04-01 Honeywell International, Inc. Start time of gyro assembly
JP2010042146A (ja) * 2008-08-13 2010-02-25 Ge Medical Systems Global Technology Co Llc 超音波撮像装置
US8156264B2 (en) * 2009-04-03 2012-04-10 Analog Devices, Inc. Digital output sensor FIFO buffer with single port memory
JP5191984B2 (ja) * 2009-12-17 2013-05-08 日本航空電子工業株式会社 リングレーザジャイロ装置
FR2958740B1 (fr) * 2010-04-13 2012-03-30 Thales Sa Dispositif de traitement numerique de l'information issue d'un gyrolaser et gyrolaser associe.
US8259302B2 (en) 2010-07-30 2012-09-04 Honeywell International Inc. Variable path length control modulation frequency
US8422022B2 (en) 2010-08-05 2013-04-16 Honeywell International Inc. Increasing the scale factor of gas laser based gyroscopes with an external gain saturation beam
JP5643584B2 (ja) * 2010-09-13 2014-12-17 日本航空電子工業株式会社 リングレーザジャイロ装置
CN102403890B (zh) * 2010-09-13 2014-05-07 立锜科技股份有限公司 频率抖动电路及其控制方法
CN102003958B (zh) * 2010-10-01 2012-07-04 中国人民解放军国防科学技术大学 四频激光陀螺工作点的控制装置
US8687198B2 (en) 2011-09-20 2014-04-01 Honeywell International Inc. Coupled cavity dispersion enhanced ring laser gyroscope
US8901432B2 (en) 2011-09-30 2014-12-02 Honeywell International Inc. Mitigation of block bending in a ring laser gyroscope caused by thermal expansion or compression of a circuit board
US8905635B2 (en) 2011-09-30 2014-12-09 Honeywell International Inc. Temperature sensor attachment facilitating thermal conductivity to a measurement point and insulation from a surrounding environment
US8781778B2 (en) * 2011-09-30 2014-07-15 Honeywell International Inc. Systems and methods for thermal gradient compensation for ring laser gyroscopes
US9091598B2 (en) 2011-09-30 2015-07-28 Honeywell International Inc. Circuits for determining differential and average temperatures from resistive temperature devices
US20130088827A1 (en) * 2011-10-07 2013-04-11 Frontier Electronic Systems Corp. Multi-Purpose Display Platform
US8604953B2 (en) * 2011-11-14 2013-12-10 Analog Devices, Inc. Calibrating timing, gain and bandwidth mismatch in interleaved ADCs
TWI416070B (zh) * 2011-12-26 2013-11-21 Ind Tech Res Inst 陀螺儀的讀取電路
TWI532323B (zh) 2013-08-14 2016-05-01 財團法人工業技術研究院 數位脈波寬度產生器及其產生方法
US9671228B2 (en) * 2014-10-21 2017-06-06 Honeywell International Inc. Floating current mirror for RLG discharge control
JP6129257B2 (ja) * 2015-09-02 2017-05-17 三菱電機株式会社 ディザ電流給電制御方法及びディザ電流給電制御装置
CN107167125B (zh) * 2017-07-05 2023-06-02 陕西蔚蓝航天测控技术开发有限公司 一种抖动激光陀螺老炼电源控制系统及抖动激光陀螺老炼电源控制机箱
CN108106615B (zh) * 2017-12-08 2023-07-28 中船重工西安东仪科工集团有限公司 一种可设定初始航向的水下mems航向陀螺
KR101978488B1 (ko) * 2017-12-27 2019-05-14 주식회사 한화 링 레이저 자이로스코프의 실행 주기를 제어하는 장치 및 그 방법
KR102027525B1 (ko) * 2018-12-13 2019-10-01 주식회사 한화 플라즈마 분광을 이용하여 링 레이저 내부의 기체의 압력 변화를 측정하는 링 레이저 자이로스코프
CN110440781A (zh) * 2019-06-21 2019-11-12 西安德讯威光电测控技术有限公司 一种用于激光陀螺的高压电源
RU2731656C1 (ru) * 2019-07-31 2020-09-07 Публичное акционерное общество "Московский институт электромеханики и автоматики" (ПАО "МИЭА") Инерциальное измерительное устройство с цифровым средством управления
CN111141267B (zh) * 2019-12-31 2021-10-22 中国船舶重工集团公司第七一七研究所 一种机抖激光陀螺仪抖动控制系统抗干扰的方法
CN111623804B (zh) * 2020-07-21 2021-10-29 湖南智航联测科技有限公司 一种激光陀螺测试系统及其测试方法
CN114577194B (zh) * 2021-12-21 2022-12-16 北京神导科技股份有限公司 一种新型二频机抖激光陀螺信号解调系统和方法
CN115290124B (zh) * 2022-10-10 2022-12-13 天津集智航宇科技有限公司 一种激光陀螺无转动出光真空老练装置及方法
CN115406468B (zh) * 2022-11-01 2023-01-17 天津集智航宇科技有限公司 基于机械纳米步进调节激光陀螺的背向散射的装置和方法
CN115603612B (zh) * 2022-12-14 2023-03-14 西安航天精密机电研究所 一种宇航用陀螺仪启停方法

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4299490A (en) * 1978-12-07 1981-11-10 Mcdonnell Douglas Corporation Phase nulling optical gyro
US4282495A (en) * 1979-05-29 1981-08-04 The Singer Company High efficiency current regulator for ring laser gyroscope
US4755057A (en) * 1984-10-02 1988-07-05 Litton Systems, Inc. Path length control method for ring laser gyroscope
KR930003178B1 (ko) 1990-06-29 1993-04-23 삼성전자주식회사 상관적응형 휘도신호와 색신호 분리회로
US5100235A (en) * 1990-07-24 1992-03-31 Honeywell Inc. Laser-ring gyro beam intensity monitor
US5249031A (en) 1991-12-11 1993-09-28 Honeywell Inc. Ring laser gyro dither stripper
US5390019A (en) 1992-07-17 1995-02-14 Honeywell Inc. Laser gyro built in test method and apparatus
US5406369A (en) 1992-07-17 1995-04-11 Honeywell Inc. Laser gyro microprocessor configuration and control
US5363194A (en) 1992-08-18 1994-11-08 Honeywell Inc. Laser gyro microprocessor start up control method and apparatus
US5299211A (en) 1992-08-27 1994-03-29 Honeywell Inc. Laser gyro high voltage start module and high voltage pulse generator
US5371754A (en) 1993-01-26 1994-12-06 Honeywell Inc. Laser gyro single transformer power supply

Also Published As

Publication number Publication date
AU1213995A (en) 1995-06-13
BR9408186A (pt) 1997-08-26
AU699978B2 (en) 1998-12-17
WO1995014906A2 (en) 1995-06-01
CN1145664A (zh) 1997-03-19
EP0733196A1 (en) 1996-09-25
JPH09505668A (ja) 1997-06-03
NO962183D0 (no) 1996-05-29
WO1995014906A3 (en) 1995-07-27
KR960706629A (ko) 1996-12-09
NO962183L (no) 1996-07-26
US6208414B1 (en) 2001-03-27
CA2176752A1 (en) 1995-06-01

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