CA2517018A1 - Method for measuring force-dependent gyroscope sensitivity - Google Patents

Method for measuring force-dependent gyroscope sensitivity Download PDF

Info

Publication number
CA2517018A1
CA2517018A1 CA002517018A CA2517018A CA2517018A1 CA 2517018 A1 CA2517018 A1 CA 2517018A1 CA 002517018 A CA002517018 A CA 002517018A CA 2517018 A CA2517018 A CA 2517018A CA 2517018 A1 CA2517018 A1 CA 2517018A1
Authority
CA
Canada
Prior art keywords
force
instrument
effect model
rotations
state diagram
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.)
Abandoned
Application number
CA002517018A
Other languages
English (en)
French (fr)
Inventor
G. Kevin Liu
John Mark
Daniel A. Tazartes
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Northrop Grumman Corp
Original Assignee
Individual
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Publication of CA2517018A1 publication Critical patent/CA2517018A1/en
Abandoned legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01CMEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C21/00Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00
    • G01C21/10Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration
    • G01C21/12Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning
    • G01C21/16Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning by integrating acceleration or speed, i.e. inertial navigation
    • G01C21/183Compensation of inertial measurements, e.g. for temperature effects
    • G01C21/188Compensation of inertial measurements, e.g. for temperature effects for accumulated errors, e.g. by coupling inertial systems with absolute positioning systems
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01CMEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C25/00Manufacturing, calibrating, cleaning, or repairing instruments or devices referred to in the other groups of this subclass
    • G01C25/005Manufacturing, calibrating, cleaning, or repairing instruments or devices referred to in the other groups of this subclass initial alignment, calibration or starting-up of inertial devices

Landscapes

  • Engineering & Computer Science (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Manufacturing & Machinery (AREA)
  • Gyroscopes (AREA)
  • Force Measurement Appropriate To Specific Purposes (AREA)
CA002517018A 2003-03-17 2003-11-12 Method for measuring force-dependent gyroscope sensitivity Abandoned CA2517018A1 (en)

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 (1)

Publication Number Publication Date
CA2517018A1 true CA2517018A1 (en) 2004-09-30

Family

ID=32987488

Family Applications (1)

Application Number Title Priority Date Filing Date
CA002517018A Abandoned CA2517018A1 (en) 2003-03-17 2003-11-12 Method for measuring force-dependent gyroscope sensitivity

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)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN115208760A (zh) * 2022-07-14 2022-10-18 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、介质及程序产品

Families Citing this family (21)

* Cited by examiner, † Cited by third party
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

Family Cites Families (13)

* Cited by examiner, † Cited by third party
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

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN115208760A (zh) * 2022-07-14 2022-10-18 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、介质及程序产品
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

Also Published As

Publication number Publication date
AU2003287627A1 (en) 2004-10-11
JP4929445B2 (ja) 2012-05-09
WO2004083782A1 (en) 2004-09-30
EP1604173A1 (en) 2005-12-14
JP2006514294A (ja) 2006-04-27
IL170574A (en) 2010-12-30
US6904377B2 (en) 2005-06-07
US20040186676A1 (en) 2004-09-23
EP1604173B1 (en) 2012-09-26
EP1604173B8 (en) 2012-10-31

Similar Documents

Publication Publication Date Title
US6904377B2 (en) Method for measuring force-dependent gyroscope sensitivity
CN104736963B (zh) 测绘系统和方法
CA2381196C (en) Vibration compensation for sensors
US6516283B2 (en) Core inertial measurement unit
US7142983B2 (en) Method for the processing of non-continuous atom interferometer intertial instrument measurements and continuous wide bandwidth instrument measurements with a gravity database
US6494093B2 (en) Method of measuring motion
CN110887507B (zh) 一种快速估计惯性测量单元全部零偏的方法
KR101739390B1 (ko) 중력오차보상을 통한 관성항법장치의 자체정렬 정확도 향상기법
CN112964240B (zh) 一种连续寻北装置、方法、电子设备及存储介质
CN116067394A (zh) 一种系统性调制惯导系统误差的方法及终端
Elwell Inertial navigation for the urban warrior
CN113155114B (zh) Mems惯性测量单元陀螺零位的温度补偿方法及装置
CN113465599B (zh) 定位定向方法、装置及系统
CN111678538A (zh) 一种基于速度匹配的动态水平仪误差补偿方法
CN106153042A (zh) 航向角获取方法和装置
JP2018052489A (ja) 機首方位測定システムにおけるセンサ測定の欠如を補償するシステムと方法
MX2013007863A (es) Reducir contribuciones de error a mediciones giroscopicas.
CN117203493A (zh) 辅助车辆的导航的方法
RU2711572C1 (ru) Способ автономного определения уходов платформы трехосного гиростабилизатора
DEYST JR et al. Strapdown inertial system alignment using statistical filters-A simplified formulation.
CN113624251A (zh) 用于矿用惯导系统的高精度标定方法
Schwarz Inertial Surveying Systems—Experience and Prognosis
Ben-Ishai et al. Kalman filter mechanization in INS/Seeker fusion and observability analysis
Xiangjin et al. Research and experiment on system level calibration method of fiber optic strapdown inertial navigation system
RU2779274C1 (ru) Способ измерения ошибок начальной выставки инерциальной навигационной системы без привязки к внешним ориентирам

Legal Events

Date Code Title Description
EEER Examination request
FZDE Discontinued