DE69306967T2 - Dreieckige vibrationen erzeugende steuervorrichtung für einen ringlaserkreisel - Google Patents

Dreieckige vibrationen erzeugende steuervorrichtung für einen ringlaserkreisel

Info

Publication number
DE69306967T2
DE69306967T2 DE69306967T DE69306967T DE69306967T2 DE 69306967 T2 DE69306967 T2 DE 69306967T2 DE 69306967 T DE69306967 T DE 69306967T DE 69306967 T DE69306967 T DE 69306967T DE 69306967 T2 DE69306967 T2 DE 69306967T2
Authority
DE
Germany
Prior art keywords
gym
control device
vibration generating
generating control
ring laser
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 - Fee Related
Application number
DE69306967T
Other languages
English (en)
Other versions
DE69306967D1 (de
Inventor
Andrew Karpinski
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
Publication of DE69306967D1 publication Critical patent/DE69306967D1/de
Application granted granted Critical
Publication of DE69306967T2 publication Critical patent/DE69306967T2/de
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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
    • G01C19/68—Lock-in prevention
    • G01C19/70—Lock-in prevention by mechanical means

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)
  • Control Of Stepping Motors (AREA)
DE69306967T 1992-09-30 1993-09-30 Dreieckige vibrationen erzeugende steuervorrichtung für einen ringlaserkreisel Expired - Fee Related DE69306967T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US07/954,082 US5341209A (en) 1992-09-30 1992-09-30 Triangular dither drive apparatus for a ring laser gyroscope
PCT/US1993/009316 WO1994008206A1 (en) 1992-09-30 1993-09-30 Triangular dither drive apparatus for a ring laser gyroscope

Publications (2)

Publication Number Publication Date
DE69306967D1 DE69306967D1 (de) 1997-02-06
DE69306967T2 true DE69306967T2 (de) 1997-06-12

Family

ID=25494896

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69306967T Expired - Fee Related DE69306967T2 (de) 1992-09-30 1993-09-30 Dreieckige vibrationen erzeugende steuervorrichtung für einen ringlaserkreisel

Country Status (5)

Country Link
US (1) US5341209A (de)
EP (1) EP0663064B1 (de)
JP (1) JP3411034B2 (de)
DE (1) DE69306967T2 (de)
WO (1) WO1994008206A1 (de)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6718823B2 (en) * 2002-04-30 2004-04-13 Honeywell International Inc. Pulse width modulation drive signal for a MEMS gyroscope
US7486042B2 (en) * 2006-07-05 2009-02-03 Honeywell International Inc. Component position determination circuit using a brushless DC motor commutation sensor
FR2958740B1 (fr) * 2010-04-13 2012-03-30 Thales Sa Dispositif de traitement numerique de l'information issue d'un gyrolaser et gyrolaser associe.
KR101475799B1 (ko) * 2013-11-05 2014-12-24 국방과학연구소 링 레이저 자이로의 각진동 신호 이중 복조 방법

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3373650A (en) * 1965-04-02 1968-03-19 Honeywell Inc Laser angular rate sensor
US4152071A (en) * 1976-08-02 1979-05-01 Honeywell Inc. Control apparatus
US4445779A (en) * 1981-07-06 1984-05-01 Honeywell Inc. Dither system for a spring mass system
DE3150160A1 (de) * 1981-12-18 1983-06-30 Honeywell Gmbh, 6050 Offenbach Ringlaserkreisel
US4790658A (en) * 1985-05-24 1988-12-13 Honeywell Inc. Dither signal remover for a dithered ring laser angular rate sensor
US4826320A (en) * 1985-05-24 1989-05-02 Honeywell Inc. Dither signal remover for a dithered ring laser angular rate sensor
US4898469A (en) * 1985-05-24 1990-02-06 Sewell Wesley C Dither signal remover for a dithered ring laser angular rate sensor
US4988908A (en) * 1989-05-31 1991-01-29 Honeywell Inc. Piezoelectric transducers for a ring laser gyroscope dither motor
US5094537A (en) * 1991-03-08 1992-03-10 Honeywell Inc. Signal processing system for correcting ring laser gyroscope readout

Also Published As

Publication number Publication date
DE69306967D1 (de) 1997-02-06
WO1994008206A1 (en) 1994-04-14
EP0663064B1 (de) 1996-12-27
EP0663064A1 (de) 1995-07-19
JP3411034B2 (ja) 2003-05-26
US5341209A (en) 1994-08-23
JPH08502356A (ja) 1996-03-12

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee