JP2006514294A5 - - Google Patents

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Publication number
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
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Japan
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force
error
path
hatemo
parameters
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JP2004569683A
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Japanese (ja)
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JP4929445B2 (ja
JP2006514294A (ja
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Priority claimed from US10/390,200 external-priority patent/US6904377B2/en
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Publication of JP2006514294A5 publication Critical patent/JP2006514294A5/ja
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Publication of JP4929445B2 publication Critical patent/JP4929445B2/ja
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JP2004569683A 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 Expired - Lifetime JP4929445B2 (ja)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US10/390,200 2003-03-17
US10/390,200 US6904377B2 (en) 2003-03-17 2003-03-17 Method for measuring force-dependent gyroscope sensitivity
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 (https=) 2011-06-30
JP4929445B2 JP4929445B2 (ja) 2012-05-09

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Family Applications (1)

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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 (https=)
EP (1) EP1604173B8 (https=)
JP (1) JP4929445B2 (https=)
AU (1) AU2003287627A1 (https=)
CA (1) CA2517018A1 (https=)
IL (1) IL170574A (https=)
WO (1) WO2004083782A1 (https=)

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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
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US20060250257A1 (en) * 2005-05-09 2006-11-09 Reynolds Christopher I Sensor orientation for environmental error reduction
US8548766B2 (en) 2009-09-14 2013-10-01 Honeywell International Inc. Systems and methods for gyroscope calibration
US8108171B2 (en) * 2009-09-14 2012-01-31 Honeywell International, Inc. Systems and methods for calibration of gyroscopes and a magnetic compass
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
US20170323240A1 (en) 2016-05-06 2017-11-09 General Electric Company Computing system to control the use of physical state attainment with inspection
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

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