CA2009788A1 - Computer Generated Dither Drive - Google Patents
Computer Generated Dither DriveInfo
- Publication number
- CA2009788A1 CA2009788A1 CA2009788A CA2009788A CA2009788A1 CA 2009788 A1 CA2009788 A1 CA 2009788A1 CA 2009788 A CA2009788 A CA 2009788A CA 2009788 A CA2009788 A CA 2009788A CA 2009788 A1 CA2009788 A1 CA 2009788A1
- Authority
- CA
- Canada
- Prior art keywords
- flexure
- dither drive
- dither
- frame
- signal
- 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
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
Abstract
A dither drive system for a ring laser gyroscope includes a computer, a digital to analog converter, a filter and a power amplifier. The system also includes a frame mounted to a flexure having a resonant frequency, the flexure being mounted between a base and the frame such that the frame may be dithered relative to the base.
The dither frequency is sensed and a digital signal that corresponds to a specified dither drive signal is produced.
The digital signal is converted to a corresponding analog signal and the dither drive signal is toggled to drive the flexure at its resonant frequency. This system avoids the necessity of using much of the expensive hardware included in previous systems.
The dither frequency is sensed and a digital signal that corresponds to a specified dither drive signal is produced.
The digital signal is converted to a corresponding analog signal and the dither drive signal is toggled to drive the flexure at its resonant frequency. This system avoids the necessity of using much of the expensive hardware included in previous systems.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US07/367,957 US4981359A (en) | 1989-06-19 | 1989-06-19 | Ring laser gyroscope dither drive system and method |
US367,957 | 1989-06-19 |
Publications (2)
Publication Number | Publication Date |
---|---|
CA2009788A1 true CA2009788A1 (en) | 1990-12-19 |
CA2009788C CA2009788C (en) | 1999-11-23 |
Family
ID=23449305
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CA002009788A Expired - Fee Related CA2009788C (en) | 1989-06-19 | 1990-02-12 | Computer generated dither drive |
Country Status (5)
Country | Link |
---|---|
US (1) | US4981359A (en) |
JP (1) | JP2644067B2 (en) |
CA (1) | CA2009788C (en) |
FR (1) | FR2648556B1 (en) |
GB (1) | GB2233145B (en) |
Families Citing this family (39)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5473945A (en) * | 1990-02-14 | 1995-12-12 | The Charles Stark Draper Laboratory, Inc. | Micromechanical angular accelerometer with auxiliary linear accelerometer |
US5357817A (en) * | 1990-04-19 | 1994-10-25 | Charles Stark Draper Laboratory, Inc. | Wide bandwidth stable member without angular accelerometers |
US5325173A (en) * | 1990-05-04 | 1994-06-28 | Litton Systems, Inc. | Apparatus for compensating for change in laser gyro dither pickoff scale factor |
US5605598A (en) * | 1990-10-17 | 1997-02-25 | The Charles Stark Draper Laboratory Inc. | Monolithic micromechanical vibrating beam accelerometer with trimmable resonant frequency |
US5408119A (en) * | 1990-10-17 | 1995-04-18 | The Charles Stark Draper Laboratory, Inc. | Monolithic micromechanical vibrating string accelerometer with trimmable resonant frequency |
US5635639A (en) * | 1991-09-11 | 1997-06-03 | The Charles Stark Draper Laboratory, Inc. | Micromechanical tuning fork angular rate sensor |
US5331852A (en) * | 1991-09-11 | 1994-07-26 | The Charles Stark Draper Laboratory, Inc. | Electromagnetic rebalanced micromechanical transducer |
US5408877A (en) * | 1992-03-16 | 1995-04-25 | The Charles Stark Draper Laboratory, Inc. | Micromechanical gyroscopic transducer with improved drive and sense capabilities |
US5767405A (en) * | 1992-04-07 | 1998-06-16 | The Charles Stark Draper Laboratory, Inc. | Comb-drive micromechanical tuning fork gyroscope with piezoelectric readout |
US5349855A (en) * | 1992-04-07 | 1994-09-27 | The Charles Stark Draper Laboratory, Inc. | Comb drive micromechanical tuning fork gyro |
US5388458A (en) * | 1992-11-24 | 1995-02-14 | The Charles Stark Draper Laboratory, Inc. | Quartz resonant gyroscope or quartz resonant tuning fork gyroscope |
US5555765A (en) * | 1993-02-10 | 1996-09-17 | The Charles Stark Draper Laboratory, Inc. | Gimballed vibrating wheel gyroscope |
US5650568A (en) * | 1993-02-10 | 1997-07-22 | The Charles Stark Draper Laboratory, Inc. | Gimballed vibrating wheel gyroscope having strain relief features |
US5416584A (en) * | 1994-04-25 | 1995-05-16 | Honeywell Inc. | Sinusoidal noise injection into the dither of a ring laser gyroscope |
US5581035A (en) * | 1994-08-29 | 1996-12-03 | The Charles Stark Draper Laboratory, Inc. | Micromechanical sensor with a guard band electrode |
US5646348A (en) | 1994-08-29 | 1997-07-08 | The Charles Stark Draper Laboratory, Inc. | Micromechanical sensor with a guard band electrode and fabrication technique therefor |
US5725729A (en) * | 1994-09-26 | 1998-03-10 | The Charles Stark Draper Laboratory, Inc. | Process for micromechanical fabrication |
JPH0973965A (en) * | 1995-09-04 | 1997-03-18 | Sumitomo Electric Ind Ltd | Cable reel |
US5817942A (en) * | 1996-02-28 | 1998-10-06 | The Charles Stark Draper Laboratory, Inc. | Capacitive in-plane accelerometer |
US5892153A (en) * | 1996-11-21 | 1999-04-06 | The Charles Stark Draper Laboratory, Inc. | Guard bands which control out-of-plane sensitivities in tuning fork gyroscopes and other sensors |
US5911156A (en) * | 1997-02-24 | 1999-06-08 | The Charles Stark Draper Laboratory, Inc. | Split electrode to minimize charge transients, motor amplitude mismatch errors, and sensitivity to vertical translation in tuning fork gyros and other devices |
US5783973A (en) * | 1997-02-24 | 1998-07-21 | The Charles Stark Draper Laboratory, Inc. | Temperature insensitive silicon oscillator and precision voltage reference formed therefrom |
US5952574A (en) * | 1997-04-29 | 1999-09-14 | The Charles Stark Draper Laboratory, Inc. | Trenches to reduce charging effects and to control out-of-plane sensitivities in tuning fork gyroscopes and other sensors |
US6340883B1 (en) * | 1998-09-03 | 2002-01-22 | Sony/Tektronik Corporation | Wide band IQ splitting apparatus and calibration method therefor with balanced amplitude and phase between I and Q |
US6539038B1 (en) * | 2000-11-13 | 2003-03-25 | Jds Uniphase Corporation | Reference frequency quadrature phase-based control of drive level and DC bias of laser modulator |
AU2003226083A1 (en) * | 2002-03-26 | 2003-10-13 | The Charles Stark Draper Laboratory, Inc. | Microelectromechanical sensors having reduced signal bias errors and methods of manufacturing the same |
US6823733B2 (en) * | 2002-11-04 | 2004-11-30 | Matsushita Electric Industrial Co., Ltd. | Z-axis vibration gyroscope |
US7505140B2 (en) * | 2007-04-13 | 2009-03-17 | Custom Sensors & Technologies, Inc. | Indexing dithering mechanism and method |
US7548318B2 (en) * | 2007-04-13 | 2009-06-16 | Custom Sensors & Technologies, Inc. | Dithering mechanism for eliminating zero-rate bias in a gyroscope |
US8187902B2 (en) * | 2008-07-09 | 2012-05-29 | The Charles Stark Draper Laboratory, Inc. | High performance sensors and methods for forming the same |
US8259302B2 (en) | 2010-07-30 | 2012-09-04 | Honeywell International Inc. | Variable path length control modulation frequency |
US9310202B2 (en) * | 2012-07-09 | 2016-04-12 | Freescale Semiconductor, Inc. | Angular rate sensor with quadrature error compensation |
US9568318B2 (en) * | 2015-04-22 | 2017-02-14 | Honeywell International Inc. | Rotationally biased fiber optic gyroscope |
CN105093239B (en) * | 2015-08-21 | 2017-07-28 | 西安空间无线电技术研究所 | A kind of Time Delay of Systems error calibration method based on temperature-compensating |
CN106153029B (en) * | 2016-08-17 | 2019-02-12 | 中国船舶重工集团公司第七0七研究所 | Two frequency machine shaking laser gyroscope shaking signal cancellation devices |
CN112284411B (en) * | 2020-09-09 | 2023-07-28 | 北京航天时代激光导航技术有限责任公司 | Jitter control method of laser inertial measurement unit |
CN112665571B (en) * | 2020-12-01 | 2023-10-13 | 华中光电技术研究所(中国船舶重工集团公司第七一七研究所) | Embedded shaking system of laser gyro |
CN114910099B (en) * | 2022-05-27 | 2024-01-23 | 四川图林科技有限责任公司 | Method for measuring delay of mechanically-jittered laser gyro control circuit |
US11852483B1 (en) | 2022-08-12 | 2023-12-26 | Honeywell International Inc. | Dither motor apparatus with pickoff embedded drives for ring laser gyroscope |
Family Cites Families (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3373650A (en) * | 1965-04-02 | 1968-03-19 | Honeywell Inc | Laser angular rate sensor |
US3743969A (en) * | 1969-11-12 | 1973-07-03 | North American Rockwell | Modulation servo control for frequency modulated ring laser gyro |
US4255054A (en) * | 1979-03-21 | 1981-03-10 | The Singer Company | Lock-in control system for spring suspended ring laser gyroscope |
US4243324A (en) * | 1979-03-21 | 1981-01-06 | The Singer Company | Feedback system for controlling lock-in in spring suspended ring laser gyroscope |
US4248534A (en) * | 1979-05-09 | 1981-02-03 | The Singer Company | Apparatus and method for the elimination of angular vibration induced errors in ring laser gyroscopes |
US4422762A (en) * | 1979-11-05 | 1983-12-27 | Litton Systems, Inc. | Ring laser |
US4309107A (en) * | 1980-01-11 | 1982-01-05 | Litton Systems, Inc. | Laser gyro dither mechanism |
US4314174A (en) * | 1980-03-25 | 1982-02-02 | Litton Systems, Inc. | Piezoelectric transducer drive having temperature compensation |
DE3279480D1 (en) * | 1981-07-06 | 1989-04-06 | Honeywell Inc | Method and apparatus for angular rate sensing |
US4445779A (en) * | 1981-07-06 | 1984-05-01 | Honeywell Inc. | Dither system for a spring mass system |
US4529311A (en) * | 1981-07-06 | 1985-07-16 | Honeywell Inc. | Ring laser gyro system |
US4473297A (en) * | 1981-11-12 | 1984-09-25 | The Singer Company | Ring laser gyroscope utilizing phase detector for minimizing beam lock-in |
US4597667A (en) * | 1982-12-09 | 1986-07-01 | Litton Systems, Inc. | Dither controller for ring laser angular rotation sensor |
US4584652A (en) * | 1983-10-07 | 1986-04-22 | Litton Systems, Inc. | Apparatus and method for determining in-phase and quadrature-phase components |
US4801206A (en) * | 1986-06-04 | 1989-01-31 | Litton Systems, Inc. | Simplified ring laser gyroscope dither control and method |
GB8620943D0 (en) * | 1986-08-29 | 1986-10-08 | British Aerospace | Signal processing circuits |
-
1989
- 1989-06-19 US US07/367,957 patent/US4981359A/en not_active Expired - Lifetime
-
1990
- 1990-01-16 GB GB9000914A patent/GB2233145B/en not_active Expired - Fee Related
- 1990-02-12 CA CA002009788A patent/CA2009788C/en not_active Expired - Fee Related
- 1990-04-17 FR FR9004897A patent/FR2648556B1/en not_active Expired - Fee Related
- 1990-06-19 JP JP2158868A patent/JP2644067B2/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
GB2233145B (en) | 1993-12-22 |
US4981359A (en) | 1991-01-01 |
JP2644067B2 (en) | 1997-08-25 |
FR2648556A1 (en) | 1990-12-21 |
CA2009788C (en) | 1999-11-23 |
GB2233145A (en) | 1991-01-02 |
GB9000914D0 (en) | 1990-03-14 |
FR2648556B1 (en) | 1995-10-20 |
JPH0332076A (en) | 1991-02-12 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CA2009788A1 (en) | Computer Generated Dither Drive | |
AU2867389A (en) | Amplifying optical signals | |
AU3007689A (en) | Frequency conversion of optical radiation | |
AU677813B2 (en) | Image signal converter | |
GB2229597B (en) | A method and an arrangement for increasing the dynamic range at an input stage of an optical receiver | |
AU2757188A (en) | Multi-directional optical scanner | |
EP0377519A3 (en) | Modulation system capable of accurately compensating for nonlinearities of an amplifier connected thereto | |
AU3495489A (en) | Optical amplifier module | |
AU3556393A (en) | Micropower amplifier/transducer with signal expansion | |
AU1119288A (en) | Nonlinear signal generating circuit and nonlinear compensating device using the same | |
AU6755287A (en) | Vibrating beam transducer | |
AU3253389A (en) | Extensible mast support system | |
EP0331304A3 (en) | Amplification of optical signals | |
AU5833990A (en) | Optical recorder | |
AU4383693A (en) | Digital transducer system | |
GB8829333D0 (en) | Optical frequency monitor | |
GB8823250D0 (en) | Ring resonator gyroscope | |
AU2073588A (en) | Combination beam combiner and beam emitter for ring laser gyroscope | |
AU6991491A (en) | Integrated optical signal amplifier | |
AU4377189A (en) | High resolution digital line scanner | |
AU2662088A (en) | Mounting structure of a small-sized acoustic component | |
AU3997785A (en) | Ring laser gyro tilt mirror dither | |
SG22994G (en) | Optical amplifier with reduced nonlinearity | |
USRE37517E1 (en) | Portion of an optical scanner | |
AU3001189A (en) | Removal of nitrogen from iron |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
EEER | Examination request | ||
MKLA | Lapsed |