JP2005516222A5 - - Google Patents

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Publication number
JP2005516222A5
JP2005516222A5 JP2003564596A JP2003564596A JP2005516222A5 JP 2005516222 A5 JP2005516222 A5 JP 2005516222A5 JP 2003564596 A JP2003564596 A JP 2003564596A JP 2003564596 A JP2003564596 A JP 2003564596A JP 2005516222 A5 JP2005516222 A5 JP 2005516222A5
Authority
JP
Japan
Prior art keywords
computer
high acceleration
accelerometer
accelerometer output
output
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.)
Pending
Application number
JP2003564596A
Other languages
English (en)
Japanese (ja)
Other versions
JP2005516222A (ja
Filing date
Publication date
Priority claimed from US10/056,718 external-priority patent/US6826502B2/en
Application filed filed Critical
Publication of JP2005516222A publication Critical patent/JP2005516222A/ja
Publication of JP2005516222A5 publication Critical patent/JP2005516222A5/ja
Pending legal-status Critical Current

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JP2003564596A 2002-01-25 2003-01-24 バイアス不安定性を有する加速度計を訂正および較正する方法およびシステム Pending JP2005516222A (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US10/056,718 US6826502B2 (en) 2002-01-25 2002-01-25 Methods and systems for calibration and compensation of accelerometers with bias instability
PCT/US2003/002188 WO2003065054A1 (en) 2002-01-25 2003-01-24 Method and system for correction and calibration of accelerometers with bias instability

Publications (2)

Publication Number Publication Date
JP2005516222A JP2005516222A (ja) 2005-06-02
JP2005516222A5 true JP2005516222A5 (enExample) 2006-03-23

Family

ID=27609319

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2003564596A Pending JP2005516222A (ja) 2002-01-25 2003-01-24 バイアス不安定性を有する加速度計を訂正および較正する方法およびシステム

Country Status (4)

Country Link
US (1) US6826502B2 (enExample)
EP (1) EP1468299A1 (enExample)
JP (1) JP2005516222A (enExample)
WO (1) WO2003065054A1 (enExample)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2006176084A (ja) * 2004-12-24 2006-07-06 Advics:Kk 車両挙動センサの検出値補正方法
US7467536B2 (en) * 2005-11-21 2008-12-23 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Positioning system for single or multi-axis sensitive instrument calibration and calibration system for use therewith
JP4560016B2 (ja) * 2006-07-31 2010-10-13 アキム株式会社 電子部品の調整検査装置
US7643960B2 (en) * 2007-03-05 2010-01-05 Gm Global Technology Operations, Inc. Correction of factors in vehicle accelerometer signals
ITTO20070335A1 (it) 2007-05-15 2008-11-16 Sequoia It S R L Accelerometro ad ampia banda con autoriconoscimento della calibrazione
JP2008304262A (ja) 2007-06-06 2008-12-18 Freescale Semiconductor Inc 温度補償回路、トリミング回路及び加速度検出装置
US20090259424A1 (en) * 2008-03-06 2009-10-15 Texas Instruments Incorporated Parameter estimation for accelerometers, processes, circuits, devices and systems
US7650253B2 (en) * 2008-05-08 2010-01-19 L-3 Communications Corporation Accelerometer and method for error compensation
JP5257897B2 (ja) * 2009-06-01 2013-08-07 フリースケール セミコンダクター インコーポレイテッド 出力回路
DE102010028827B4 (de) * 2010-05-11 2021-07-01 Robert Bosch Gmbh Verfahren zum Abgleichen eines Beschleunigungssensors
FR2976357B1 (fr) * 2011-06-09 2014-02-14 Snecma Dispositif de qualification de jauges de deformation
US9052250B1 (en) 2012-05-04 2015-06-09 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Method of calibrating a force balance
US9340212B2 (en) 2014-04-01 2016-05-17 GM Global Technology Operations LLC System and method for estimating road grade based on an output of a longitudinal acceleration sensor in a vehicle
CN106575150B (zh) 2014-08-16 2020-03-03 谷歌有限责任公司 使用运动数据识别手势的方法和可穿戴计算设备

Family Cites Families (17)

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Publication number Priority date Publication date Assignee Title
US4372162A (en) 1981-08-13 1983-02-08 Rockwell International Corporation Three-axis accelerometer having dynamic bias compensation
US4467651A (en) * 1983-01-06 1984-08-28 Sundstrand Data Control, Inc. Method for determining acceleration
US4611304A (en) 1983-07-27 1986-09-09 Sundstrand Data Control, Inc. Transducer memory circuit
US4675820A (en) * 1984-06-14 1987-06-23 Sundstrand Data Control, Inc. Inertial reference system
US4891982A (en) 1986-06-27 1990-01-09 Sundstrand Data Control, Inc. Temperature compensation of a steady-state accelerometer
US4750363A (en) 1986-06-27 1988-06-14 Sundstrand Data Control, Inc. Temperature compensation of an accelerometer
US4812977A (en) * 1986-12-31 1989-03-14 Sundstrand Data Control, Inc. Borehole survey system utilizing strapdown inertial navigation
US5610815A (en) 1989-12-11 1997-03-11 Caterpillar Inc. Integrated vehicle positioning and navigation system, apparatus and method
US5353642A (en) 1991-02-01 1994-10-11 Kyowa Electronic Instruments, Ltd. Centrifugal type acceleration measuring device
US5505410A (en) 1994-05-23 1996-04-09 Litton Systems, Inc. Instrument calibration method including compensation of centripetal acceleration effect
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
AU5425198A (en) 1996-10-21 1998-05-29 Electronics Development Corporation Smart sensor module
AU4821399A (en) * 1998-06-12 1999-12-30 Baker Hughes Incorporated Method for magnetic survey calibration and estimation of uncertainty
DE19858621C2 (de) 1998-12-18 2001-02-01 Autoflug Gmbh Verfahren zum Verbessern der Meßwerte eines inertialen Meßsystems
US6175807B1 (en) 1999-06-09 2001-01-16 Litton Systems, Inc. Temperature compensation method for strapdown inertial navigation systems
US6498996B1 (en) * 1999-08-04 2002-12-24 Honeywell International Inc. Vibration compensation for sensors
US6622091B2 (en) * 2001-05-11 2003-09-16 Fibersense Technology Corporation Method and system for calibrating an IG/GP navigational system

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