JP2006514294A5 - - Google Patents
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- JP2006514294A5 JP2006514294A5 JP2004569683A JP2004569683A JP2006514294A5 JP 2006514294 A5 JP2006514294 A5 JP 2006514294A5 JP 2004569683 A JP2004569683 A JP 2004569683A JP 2004569683 A JP2004569683 A JP 2004569683A JP 2006514294 A5 JP2006514294 A5 JP 2006514294A5
- Authority
- JP
- Japan
- Prior art keywords
- force
- error
- path
- hatemo
- parameters
- 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
- 238000000034 method Methods 0.000 claims 15
- 230000000694 effects Effects 0.000 claims 12
- 238000010586 diagram Methods 0.000 claims 7
- 230000001419 dependent effect Effects 0.000 claims 6
- 238000005259 measurement Methods 0.000 claims 5
- 239000011159 matrix material Substances 0.000 claims 3
- 230000035945 sensitivity Effects 0.000 claims 1
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US10/390,200 US6904377B2 (en) | 2003-03-17 | 2003-03-17 | Method for measuring force-dependent gyroscope sensitivity |
| US10/390,200 | 2003-03-17 | ||
| PCT/US2003/035884 WO2004083782A1 (en) | 2003-03-17 | 2003-11-12 | Method for measuring force-dependent gyroscope sensitivity |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JP2006514294A JP2006514294A (ja) | 2006-04-27 |
| JP2006514294A5 true JP2006514294A5 (enExample) | 2011-06-30 |
| JP4929445B2 JP4929445B2 (ja) | 2012-05-09 |
Family
ID=32987488
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2004569683A Expired - Lifetime JP4929445B2 (ja) | 2003-03-17 | 2003-11-12 | 力に依存するジャイロスコープの感度を測定する方法 |
Country Status (7)
| Country | Link |
|---|---|
| US (1) | US6904377B2 (enExample) |
| EP (1) | EP1604173B8 (enExample) |
| JP (1) | JP4929445B2 (enExample) |
| AU (1) | AU2003287627A1 (enExample) |
| CA (1) | CA2517018A1 (enExample) |
| IL (1) | IL170574A (enExample) |
| WO (1) | WO2004083782A1 (enExample) |
Families Citing this family (22)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2869997B1 (fr) * | 2004-05-04 | 2006-06-23 | Commissariat Energie Atomique | Accelerometre en boucle fermee avec detection d'erreur |
| US7430460B2 (en) * | 2005-03-23 | 2008-09-30 | Price Ricardo A | Method for determining roll rate gyro bias in an attitude heading reference system |
| US20060250257A1 (en) * | 2005-05-09 | 2006-11-09 | Reynolds Christopher I | Sensor orientation for environmental error reduction |
| US7650238B2 (en) | 2005-05-09 | 2010-01-19 | Northrop Grumman Corporation | Environmental characteristic determination |
| US8108171B2 (en) * | 2009-09-14 | 2012-01-31 | Honeywell International, Inc. | Systems and methods for calibration of gyroscopes and a magnetic compass |
| US8548766B2 (en) | 2009-09-14 | 2013-10-01 | Honeywell International Inc. | Systems and methods for gyroscope calibration |
| US8977512B1 (en) * | 2011-06-17 | 2015-03-10 | Bae Systems Information And Electronic Systems Integration Inc. | Method and apparatus for alignment harmonization |
| CN102788597B (zh) * | 2012-08-16 | 2014-10-29 | 辽宁工程技术大学 | 基于空间稳定的旋转捷联惯导系统误差抑制方法 |
| CN103234560B (zh) * | 2013-05-17 | 2015-09-09 | 哈尔滨工程大学 | 一种捷联惯导系统零位标定的方法 |
| CN103575296B (zh) * | 2013-10-08 | 2016-04-20 | 北京理工大学 | 一种双轴旋转惯导系统自标定方法 |
| CN104165638B (zh) * | 2014-08-07 | 2017-02-08 | 北京理工大学 | 一种双轴旋转惯导系统多位置自主标定方法 |
| US10502585B2 (en) * | 2014-10-23 | 2019-12-10 | The Boeing Company | Gyro rate computation for an interferometric fiber optic gyro |
| KR102144539B1 (ko) * | 2014-11-05 | 2020-08-18 | 주식회사 히타치엘지 데이터 스토리지 코리아 | 거리 측정 장치 |
| CN104567932A (zh) * | 2015-01-16 | 2015-04-29 | 北京航天时代光电科技有限公司 | 一种高精度光纤陀螺惯测装置标定方法 |
| US9581444B2 (en) | 2015-06-29 | 2017-02-28 | International Business Machines Corporation | Electronic roll pitch and yaw sensor using conductive fluid |
| US20170323239A1 (en) | 2016-05-06 | 2017-11-09 | General Electric Company | Constrained time computing control system to simulate and optimize aircraft operations with dynamic thermodynamic state and asset utilization attainment |
| CN110006450B (zh) * | 2019-04-15 | 2021-06-08 | 哈尔滨工业大学 | 一种激光捷联惯导系统在卧式三轴转台上的标定方法 |
| CN110108300B (zh) * | 2019-05-10 | 2021-07-13 | 哈尔滨工业大学 | 一种基于卧式三轴转台的imu正六面体标定方法 |
| CN111637883B (zh) * | 2020-04-28 | 2022-04-12 | 北京航天控制仪器研究所 | 基于速度和位置误差闭环反馈的提高惯性制导精度的方法 |
| CN113776560B (zh) * | 2021-09-17 | 2023-07-14 | 北京控制工程研究所 | 一种基于高精度三轴转台的陀螺标度因数测试方法 |
| CN114485728A (zh) * | 2022-01-04 | 2022-05-13 | 中国煤炭科工集团太原研究院有限公司 | 一种捷联惯导系统现场快速自标定方法 |
| CN115208760B (zh) * | 2022-07-14 | 2024-02-27 | 上海移为通信技术股份有限公司 | 运动检测芯片的配置方法、装置及介质 |
Family Cites Families (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CA1061132A (en) * | 1974-11-29 | 1979-08-28 | Theodore Mairson | Apparatus for performing inertial measurements using translational acceleration transducers and for calibrating translational acceleration transducers |
| US4092716A (en) * | 1975-07-11 | 1978-05-30 | Mcdonnell Douglas Corporation | Control means and method for controlling an object |
| US4060718A (en) * | 1976-12-10 | 1977-11-29 | Litton Systems, Inc. | Geodetic survey method |
| US5570304A (en) | 1994-07-27 | 1996-10-29 | Litton Systems, Inc. | Method for thermal modeling and updating of bias errors in inertial navigation instrument outputs |
| 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 |
| JPH095104A (ja) * | 1995-06-23 | 1997-01-10 | Nippon Telegr & Teleph Corp <Ntt> | 移動物体の三次元姿勢角測定法および三次元姿勢角計測装置 |
| JP2904118B2 (ja) * | 1996-05-27 | 1999-06-14 | 日本電気株式会社 | 姿勢角検出装置及び方法 |
| JP2001502063A (ja) * | 1997-06-05 | 2001-02-13 | シミュラ・インコーポレーテッド | 回転角度センサのための方法および装置 |
| US6625527B1 (en) | 1999-02-18 | 2003-09-23 | Continental Teves Ag & Co. Ohg | Sensor system with monitoring device |
| US6175807B1 (en) | 1999-06-09 | 2001-01-16 | Litton Systems, Inc. | Temperature compensation method for strapdown inertial navigation systems |
| US6760663B2 (en) * | 1999-09-14 | 2004-07-06 | Honeywell International Inc. | Solution separation method and apparatus for ground-augmented global positioning system |
| US7075914B2 (en) * | 2000-05-08 | 2006-07-11 | Microtune (San Diego), Inc. | Software modem architecture |
| US6778924B2 (en) * | 2001-11-06 | 2004-08-17 | Honeywell International Inc. | Self-calibrating inertial measurement system method and apparatus |
-
2003
- 2003-03-17 US US10/390,200 patent/US6904377B2/en not_active Expired - Lifetime
- 2003-11-12 WO PCT/US2003/035884 patent/WO2004083782A1/en not_active Ceased
- 2003-11-12 JP JP2004569683A patent/JP4929445B2/ja not_active Expired - Lifetime
- 2003-11-12 AU AU2003287627A patent/AU2003287627A1/en not_active Abandoned
- 2003-11-12 EP EP03781875A patent/EP1604173B8/en not_active Expired - Lifetime
- 2003-11-12 CA CA002517018A patent/CA2517018A1/en not_active Abandoned
-
2005
- 2005-08-30 IL IL170574A patent/IL170574A/en active IP Right Grant
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