DE3877622D1 - Inertialsensor. - Google Patents
Inertialsensor.Info
- Publication number
- DE3877622D1 DE3877622D1 DE8888303053T DE3877622T DE3877622D1 DE 3877622 D1 DE3877622 D1 DE 3877622D1 DE 8888303053 T DE8888303053 T DE 8888303053T DE 3877622 T DE3877622 T DE 3877622T DE 3877622 D1 DE3877622 D1 DE 3877622D1
- Authority
- DE
- Germany
- Prior art keywords
- inertial sensor
- inertial
- sensor
- 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
Links
Classifications
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01S—DEVICES USING THE PROCESS OF LIGHT AMPLIFICATION BY STIMULATED EMISSION OF RADIATION [LASER] TO AMPLIFY OR GENERATE LIGHT; DEVICES USING STIMULATED EMISSION OF ELECTROMAGNETIC RADIATION IN WAVE RANGES OTHER THAN OPTICAL
- H01S3/00—Lasers, i.e. devices using stimulated emission of electromagnetic radiation in the infrared, visible or ultraviolet wave range
- H01S3/05—Construction or shape of optical resonators; Accommodation of active medium therein; Shape of active medium
- H01S3/08—Construction or shape of optical resonators or components thereof
- H01S3/081—Construction or shape of optical resonators or components thereof comprising three or more reflectors
- H01S3/083—Ring lasers
-
- 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
- G01C19/668—Assemblies for measuring along different axes, e.g. triads
Landscapes
- Physics & Mathematics (AREA)
- Engineering & Computer Science (AREA)
- Electromagnetism (AREA)
- Optics & Photonics (AREA)
- Plasma & Fusion (AREA)
- Power Engineering (AREA)
- General Physics & Mathematics (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Gyroscopes (AREA)
- Lasers (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US07/034,731 US4795258A (en) | 1987-04-06 | 1987-04-06 | Nonplanar three-axis ring laser gyro with shared mirror faces |
Publications (2)
Publication Number | Publication Date |
---|---|
DE3877622D1 true DE3877622D1 (de) | 1993-03-04 |
DE3877622T2 DE3877622T2 (de) | 1993-08-12 |
Family
ID=21878249
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE8888303053T Expired - Fee Related DE3877622T2 (de) | 1987-04-06 | 1988-04-06 | Inertialsensor. |
Country Status (5)
Country | Link |
---|---|
US (1) | US4795258A (de) |
EP (1) | EP0292106B1 (de) |
JP (1) | JPH0831638B2 (de) |
CA (1) | CA1295720C (de) |
DE (1) | DE3877622T2 (de) |
Families Citing this family (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO1989011632A1 (en) * | 1988-05-27 | 1989-11-30 | Honeywell Inc. | Skewed axis inertial sensor assembly |
US5371589A (en) * | 1989-05-30 | 1994-12-06 | Litton Systems, Inc. | Triaxial ring laser gyroscope with independent cavity length control |
US5100235A (en) * | 1990-07-24 | 1992-03-31 | Honeywell Inc. | Laser-ring gyro beam intensity monitor |
US5088824A (en) * | 1990-07-31 | 1992-02-18 | Honeywell Inc. | Laser beam control for a ring-laser gyro |
US5260962A (en) * | 1992-05-29 | 1993-11-09 | The United States Of America As Represented By The Secretary Of The Air Force | Compact Lightweight ring laser gyro |
US5363700A (en) * | 1992-11-17 | 1994-11-15 | Honeywell Inc. | Skewed axis inertial sensor assembly |
US5757490A (en) * | 1996-07-31 | 1998-05-26 | Litton Systems, Inc. | Compact three-axis ring laser gyroscope |
US5932805A (en) * | 1997-08-01 | 1999-08-03 | Litton Systems, Inc. | Multisensor with directly coupled rotors |
US5932803A (en) * | 1997-08-01 | 1999-08-03 | Litton Systems, Inc. | Counterbalanced triaxial multisensor with resonant accelerometers |
US6595056B2 (en) | 2001-02-07 | 2003-07-22 | Litton Systems, Inc | Micromachined silicon gyro using tuned accelerometer |
US6474160B1 (en) | 2001-05-24 | 2002-11-05 | Northrop Grumman Corporation | Counterbalanced silicon tuned multiple accelerometer-gyro |
US6619121B1 (en) | 2001-07-25 | 2003-09-16 | Northrop Grumman Corporation | Phase insensitive quadrature nulling method and apparatus for coriolis angular rate sensors |
US20070133001A1 (en) * | 2001-09-12 | 2007-06-14 | Honeywell International Inc. | Laser sensor having a block ring activity |
FR2902870B1 (fr) * | 2006-06-23 | 2008-09-05 | Thales Sa | Dispositif d'amelioration de la duree de vie d'un gyrometre triaxial |
JP5007799B2 (ja) * | 2006-12-21 | 2012-08-22 | 株式会社Ihi | 3次元ディスクレーザ |
US8269972B2 (en) | 2010-06-29 | 2012-09-18 | Honeywell International Inc. | Beam intensity detection in a cavity ring down sensor |
US8437000B2 (en) | 2010-06-29 | 2013-05-07 | Honeywell International Inc. | Multiple wavelength cavity ring down gas sensor |
US8322191B2 (en) | 2010-06-30 | 2012-12-04 | Honeywell International Inc. | Enhanced cavity for a photoacoustic gas sensor |
CN104833790B (zh) * | 2015-05-06 | 2016-05-11 | 黑龙江科技大学 | 一种实验垮落体装置 |
Family Cites Families (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3862803A (en) * | 1968-09-27 | 1975-01-28 | United Aircraft Corp | Differential laser gyro system |
US3741657A (en) * | 1971-03-03 | 1973-06-26 | Raytheon Co | Laser gyroscope |
US4548501A (en) * | 1978-01-03 | 1985-10-22 | Raytheon Company | Laser gyroscope system |
US4229106A (en) * | 1978-05-18 | 1980-10-21 | Raytheon Company | Electromagnetic wave ring resonator |
US4247832A (en) * | 1978-12-26 | 1981-01-27 | Litton Systems, Inc. | Isotropic nonplanar ring laser |
FR2512198A1 (fr) * | 1980-03-21 | 1983-03-04 | Sfena | Gyrometre laser triaxial, monobloc, compact a six miroirs |
GB2076213B (en) * | 1980-05-09 | 1983-08-17 | Sperry Ltd | Ring laser gyroscopes |
US4397027A (en) * | 1981-01-05 | 1983-08-02 | Raytheon Company | Self-compensating gas discharge path for laser gyro |
US4477188A (en) * | 1982-04-16 | 1984-10-16 | The Singer Company | Monolithic three axis ring laser gyroscope |
US4839903A (en) * | 1985-06-27 | 1989-06-13 | British Aerospace Public Limited Company | Ring laser gyroscopes |
-
1987
- 1987-04-06 US US07/034,731 patent/US4795258A/en not_active Expired - Fee Related
-
1988
- 1988-04-06 JP JP63083218A patent/JPH0831638B2/ja not_active Expired - Lifetime
- 1988-04-06 CA CA000563453A patent/CA1295720C/en not_active Expired - Fee Related
- 1988-04-06 EP EP88303053A patent/EP0292106B1/de not_active Expired - Lifetime
- 1988-04-06 DE DE8888303053T patent/DE3877622T2/de not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
EP0292106A3 (en) | 1990-08-16 |
EP0292106A2 (de) | 1988-11-23 |
DE3877622T2 (de) | 1993-08-12 |
EP0292106B1 (de) | 1993-01-20 |
JPH0831638B2 (ja) | 1996-03-27 |
CA1295720C (en) | 1992-02-11 |
US4795258A (en) | 1989-01-03 |
JPS63308982A (ja) | 1988-12-16 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition | ||
8328 | Change in the person/name/address of the agent |
Free format text: PATENTANWAELTE MUELLER & HOFFMANN, 81667 MUENCHEN |
|
8339 | Ceased/non-payment of the annual fee |