JP2009505062A5 - - Google Patents
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- Publication number
- JP2009505062A5 JP2009505062A5 JP2008525993A JP2008525993A JP2009505062A5 JP 2009505062 A5 JP2009505062 A5 JP 2009505062A5 JP 2008525993 A JP2008525993 A JP 2008525993A JP 2008525993 A JP2008525993 A JP 2008525993A JP 2009505062 A5 JP2009505062 A5 JP 2009505062A5
- Authority
- JP
- Japan
- Prior art keywords
- signal
- bias
- inertial
- correction signal
- bias correction
- 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
- 238000005259 measurement Methods 0.000 claims 25
- 238000001514 detection method Methods 0.000 claims 7
- 238000000034 method Methods 0.000 claims 7
- 230000014509 gene expression Effects 0.000 claims 1
Applications Claiming Priority (5)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US70662805P | 2005-08-08 | 2005-08-08 | |
| US60/706,628 | 2005-08-08 | ||
| US11/364,316 | 2006-02-28 | ||
| US11/364,316 US7103477B1 (en) | 2005-08-08 | 2006-02-28 | Self-calibration for an inertial instrument based on real time bias estimator |
| PCT/US2006/021064 WO2007018689A1 (en) | 2005-08-08 | 2006-05-31 | Self-calibration for an inertial instrument based on real time bias estimator |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JP2009505062A JP2009505062A (ja) | 2009-02-05 |
| JP2009505062A5 true JP2009505062A5 (enExample) | 2009-06-04 |
| JP5243956B2 JP5243956B2 (ja) | 2013-07-24 |
Family
ID=36939577
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2008525993A Active JP5243956B2 (ja) | 2005-08-08 | 2006-05-31 | リアルタイムバイアス推定器に基づく慣性機器のための自己較正 |
Country Status (6)
| Country | Link |
|---|---|
| US (1) | US7103477B1 (enExample) |
| EP (1) | EP1913337B1 (enExample) |
| JP (1) | JP5243956B2 (enExample) |
| AT (1) | ATE435416T1 (enExample) |
| DE (1) | DE602006007589D1 (enExample) |
| WO (1) | WO2007018689A1 (enExample) |
Families Citing this family (21)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7739896B2 (en) * | 2007-03-15 | 2010-06-22 | Northrop Grumman Guidance And Electronics Company, Inc. | Self-calibration of scale factor for dual resonator class II coriolis vibratory gyros |
| US7640786B2 (en) * | 2007-03-28 | 2010-01-05 | Northrop Grumman Guidance And Electronics Company, Inc. | Self-calibrating accelerometer |
| US7698082B2 (en) | 2008-05-20 | 2010-04-13 | Northrop Grumman Guidance And Electronics Company, Inc. | Real time error determination for inertial instruments |
| US8446143B2 (en) * | 2008-06-27 | 2013-05-21 | National Instruments Corporation | Self-calibration circuit with gyrated output impedance |
| KR101008360B1 (ko) * | 2008-07-01 | 2011-01-14 | (주)마이크로인피니티 | 이동 로봇에서의 자이로 센서 오차를 교정하는 장치 및방법 |
| US7912664B2 (en) | 2008-09-11 | 2011-03-22 | Northrop Grumman Guidance And Electronics Company, Inc. | Self calibrating gyroscope system |
| US8146401B2 (en) * | 2008-09-17 | 2012-04-03 | Bae Systems Information And Electronic Systems Integration Inc. | Method and apparatus for in-flight calibration of gyroscope using magnetometer reference |
| US8011246B2 (en) * | 2008-09-22 | 2011-09-06 | Northrop Grumman Guidance And Electronics Company, Inc. | Apparatus and method for self-calibration of coriolis vibratory gyroscope |
| EP2192385A1 (en) | 2008-11-26 | 2010-06-02 | Nederlandse Organisatie voor toegepast- natuurwetenschappelijk onderzoek TNO | Signal processing module, navigation device with the signal processing module, vehicle provided with a navigation device and method of providing navigation data |
| US8095250B2 (en) * | 2009-05-21 | 2012-01-10 | Honeywell International Inc. | Real-time compensation of inertial sensor bias errors under high spin rate conditions |
| EP2504711A4 (en) * | 2009-11-24 | 2014-02-26 | Yost Engineering Inc | COMBINING REDUNDANT INERTIAL SENSORS TO CREATE A VIRTUAL SENSOR OUTPUT |
| FR3000219B1 (fr) * | 2012-12-26 | 2015-01-09 | Sagem Defense Securite | Procede de comparaison de deux centrales inertielles solidaires d'un meme porteur |
| US9651399B2 (en) | 2015-03-25 | 2017-05-16 | Northrop Grumman Systems Corporation | Continuous calibration of an inertial system |
| US9933262B2 (en) | 2015-07-27 | 2018-04-03 | Caterpillar Inc. | Positioning system having a master-slave configuration |
| US10466067B2 (en) | 2017-01-19 | 2019-11-05 | The Boeing Company | System and method for gyro rate computation for a Coriolis Vibrating Gyroscope |
| CN109000836A (zh) * | 2017-06-07 | 2018-12-14 | 北京信息科技大学 | 一种高动态载体环境力测量方法 |
| US11275099B1 (en) | 2018-07-20 | 2022-03-15 | Hrl Laboratories, Llc | Navigational grade resonant MicroElectroMechanical Systems (mems) accelerometer and method of operation |
| US11493534B1 (en) | 2019-01-04 | 2022-11-08 | Hrl Laboratories, Llc | Continuous online self-calibrating resonant FM microelectromechanical systems (MEMS) accelerometer |
| FR3107151B1 (fr) * | 2020-02-06 | 2022-12-16 | Sigfox | Procédé de récupération du temps symbole par un dispositif récepteur |
| US11841243B1 (en) | 2022-02-09 | 2023-12-12 | Hrl Laboratories, Llc | Frequency multiplexed operation of vibratory gyroscopes for continuous self-calibration |
| US11835339B1 (en) | 2022-04-05 | 2023-12-05 | Hrl Laboratories, Llc | Continuous online self-calibration for gyroscopes through modulation of damping axes |
Family Cites Families (16)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5012424A (en) * | 1989-02-22 | 1991-04-30 | Honeywell Inc. | Multiple sensor system and method |
| US5272815A (en) | 1990-11-14 | 1993-12-28 | Tokimec Inc. | Gyro compass |
| US5562266A (en) | 1992-10-29 | 1996-10-08 | Aerospatiale Societe Nationale Industrielle | Rate gyro calibration method and apparatus for a three-axis stabilized satellite |
| US5527003A (en) | 1994-07-27 | 1996-06-18 | Litton Systems, Inc. | Method for in-field updating of the gyro thermal calibration of an intertial navigation system |
| US5902351A (en) * | 1995-08-24 | 1999-05-11 | The Penn State Research Foundation | Apparatus and method for tracking a vehicle |
| WO1998049577A2 (en) | 1997-04-07 | 1998-11-05 | Motorola Inc. | Methods for gyro bias estimation using gps |
| US6678631B2 (en) * | 1998-11-19 | 2004-01-13 | Delphi Technologies, Inc. | Vehicle attitude angle estimator and method |
| SE9900113L (sv) | 1999-01-18 | 2000-05-02 | Saab Ab | Metod och anordning för att beräkna reservattityd och reservkurs för ett flygplan |
| AU5609800A (en) | 1999-06-09 | 2000-12-28 | Ipmobile Incorporated | Method and system for dynamic soft handoff resource allocation in a wireless network |
| US6498996B1 (en) | 1999-08-04 | 2002-12-24 | Honeywell International Inc. | Vibration compensation for sensors |
| US6282496B1 (en) * | 1999-10-29 | 2001-08-28 | Visteon Technologies, Llc | Method and apparatus for inertial guidance for an automobile navigation system |
| JP2001141507A (ja) * | 1999-11-11 | 2001-05-25 | Yokogawa Denshikiki Co Ltd | 慣性航法装置 |
| US6477465B1 (en) * | 1999-11-29 | 2002-11-05 | American Gnc Corporation | Vehicle self-carried positioning method and system thereof |
| US6401036B1 (en) | 2000-10-03 | 2002-06-04 | Motorola, Inc. | Heading and position error-correction method and apparatus for vehicle navigation systems |
| US6515618B1 (en) * | 2000-11-29 | 2003-02-04 | Trimble Navigation Ltd. | Fault detection and exclusion in a positioning system receiver |
| US6577952B2 (en) * | 2001-01-08 | 2003-06-10 | Motorola, Inc. | Position and heading error-correction method and apparatus for vehicle navigation systems |
-
2006
- 2006-02-28 US US11/364,316 patent/US7103477B1/en active Active
- 2006-05-31 EP EP06771696A patent/EP1913337B1/en active Active
- 2006-05-31 JP JP2008525993A patent/JP5243956B2/ja active Active
- 2006-05-31 WO PCT/US2006/021064 patent/WO2007018689A1/en not_active Ceased
- 2006-05-31 DE DE602006007589T patent/DE602006007589D1/de active Active
- 2006-05-31 AT AT06771696T patent/ATE435416T1/de not_active IP Right Cessation
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