DE602005027773D1 - Fehlerkorrektur für ein Inertialnavigationssystem - Google Patents
Fehlerkorrektur für ein InertialnavigationssystemInfo
- Publication number
- DE602005027773D1 DE602005027773D1 DE602005027773T DE602005027773T DE602005027773D1 DE 602005027773 D1 DE602005027773 D1 DE 602005027773D1 DE 602005027773 T DE602005027773 T DE 602005027773T DE 602005027773 T DE602005027773 T DE 602005027773T DE 602005027773 D1 DE602005027773 D1 DE 602005027773D1
- Authority
- DE
- Germany
- Prior art keywords
- error correction
- navigation system
- inertial navigation
- inertial
- 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.)
- Active
Links
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C21/00—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00
- G01C21/10—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration
- G01C21/12—Navigation; 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
- G01C21/16—Navigation; 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
- G01C21/183—Compensation of inertial measurements, e.g. for temperature effects
- G01C21/185—Compensation of inertial measurements, e.g. for temperature effects for gravity
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C21/00—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00
- G01C21/10—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration
- G01C21/12—Navigation; 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
- G01C21/16—Navigation; 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
- G01C21/183—Compensation of inertial measurements, e.g. for temperature effects
- G01C21/188—Compensation of inertial measurements, e.g. for temperature effects for accumulated errors, e.g. by coupling inertial systems with absolute positioning systems
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C25/00—Manufacturing, calibrating, cleaning, or repairing instruments or devices referred to in the other groups of this subclass
- G01C25/005—Manufacturing, 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
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US55706504P | 2004-03-29 | 2004-03-29 |
Publications (1)
Publication Number | Publication Date |
---|---|
DE602005027773D1 true DE602005027773D1 (de) | 2011-06-16 |
Family
ID=34886342
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE602005027773T Active DE602005027773D1 (de) | 2004-03-29 | 2005-03-29 | Fehlerkorrektur für ein Inertialnavigationssystem |
Country Status (5)
Country | Link |
---|---|
US (2) | US7509216B2 (de) |
EP (2) | EP2259023B8 (de) |
JP (1) | JP4989035B2 (de) |
CA (1) | CA2502340C (de) |
DE (1) | DE602005027773D1 (de) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2782334C1 (ru) * | 2022-01-21 | 2022-10-25 | Акционерное общество "Инерциальные технологии "Технокомплекса" (АО "ИТТ") | Способ определения параметров ориентации объекта при помощи полуаналитической инерциальной навигационной системы с географической ориентацией осей четырехосной гироплатформы |
Families Citing this family (36)
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FR2878954B1 (fr) * | 2004-12-07 | 2007-03-30 | Sagem | Systeme de navigation inertielle hybride base sur un modele cinematique |
CN1314946C (zh) * | 2005-11-04 | 2007-05-09 | 北京航空航天大学 | 一种消除陀螺常值漂移影响的惯性测量单元混合标定方法 |
KR100711261B1 (ko) * | 2006-06-21 | 2007-04-25 | (주)마이크로인피니티 | 입력 장치의 공간 인식 방법 및 그 장치 |
US7962255B2 (en) * | 2006-12-12 | 2011-06-14 | The Boeing Company | System and method for estimating inertial acceleration bias errors |
US9651387B2 (en) * | 2007-07-05 | 2017-05-16 | Invensense, Inc. | Portable navigation system |
US8024119B2 (en) * | 2007-08-14 | 2011-09-20 | Honeywell International Inc. | Systems and methods for gyrocompass alignment using dynamically calibrated sensor data and an iterated extended kalman filter within a navigation system |
EA201290258A1 (ru) * | 2009-10-30 | 2012-12-28 | Синвент Ас | Инициализация азимута и калибровка гироскопических и инерциальных приборов для исследований ствола скважины посредством внешней навигационной системы |
KR101833217B1 (ko) | 2011-12-07 | 2018-03-05 | 삼성전자주식회사 | 자기장 지도 기반 측위 시스템에서 이용되는 이동 단말 및 이를 이용한 위치 추정 방법 |
US8812233B2 (en) * | 2011-12-27 | 2014-08-19 | Caterpillar Inc. | Error detection for inertial measurement units |
CN103017787A (zh) * | 2012-07-03 | 2013-04-03 | 哈尔滨工程大学 | 适用于摇摆晃动基座的初始对准方法 |
CN102914319B (zh) * | 2012-09-29 | 2015-09-02 | 北京航空航天大学 | 一种基于先验信息的多光纤惯组贮存期静态快速检测方法 |
CN102997919B (zh) * | 2012-11-22 | 2015-07-15 | 北京理工大学 | 采用隔离载体运动提升旋转式捷联惯导误差抑制效果的方法 |
CN103591960B (zh) * | 2013-11-13 | 2016-04-20 | 北京理工大学 | 一种基于旋转调制的静基座惯性导航系统粗对准方法 |
US9803982B2 (en) * | 2014-04-28 | 2017-10-31 | Intel Corporation | Heading estimation for determining a user's location |
US9435661B2 (en) | 2014-10-08 | 2016-09-06 | Honeywell International Inc. | Systems and methods for attitude fault detection based on air data and aircraft control settings |
US9593962B2 (en) | 2014-10-08 | 2017-03-14 | Honeywell International Inc. | Systems and methods for attitude fault detection based on integrated GNSS/inertial hybrid filter residuals |
CN105783921B (zh) * | 2014-12-17 | 2019-02-19 | 高德软件有限公司 | 一种校正汽车姿态数据的方法及装置 |
CN104897172B (zh) * | 2015-06-18 | 2018-04-13 | 南京航空航天大学 | 基于运动捕捉系统的旋转mems惯导磁航向角误差补偿方法 |
CN105021192B (zh) * | 2015-07-30 | 2018-10-09 | 华南理工大学 | 一种基于零速校正的组合导航系统的实现方法 |
US9797726B2 (en) * | 2015-08-10 | 2017-10-24 | GM Global Technology Operations LLC | Reduced-order fail-safe IMU system for active safety application |
FR3043455B1 (fr) * | 2015-11-10 | 2017-12-01 | Sagem Defense Securite | Procede d'elaboration d'une navigation et procede d'orientation d'un organe de visee a partir de cette navigation |
DE102016102797A1 (de) * | 2016-02-17 | 2017-08-17 | Rheinmetall Defence Electronics Gmbh | Sensor-Vorrichtung und Sensor-System zum Bestimmen einer Lage eines Fahrzeugs oder eines Teils des Fahrzeugs |
US9915947B1 (en) * | 2016-02-26 | 2018-03-13 | Waymo Llc | System and method for determining pose data for a vehicle |
GB2550854B (en) | 2016-05-25 | 2019-06-26 | Ge Aviat Systems Ltd | Aircraft time synchronization system |
CN106643723B (zh) * | 2016-11-07 | 2019-11-26 | 哈尔滨工程大学 | 一种无人艇安全航行船位推算方法 |
CN106979779A (zh) * | 2017-05-22 | 2017-07-25 | 深圳市靖洲科技有限公司 | 一种无人车实时姿态测量方法 |
CN109141418B (zh) * | 2018-09-27 | 2022-05-13 | 东南大学 | 过载环境下捷联惯导数据处理装置及其多源误差建模方法 |
CN111044075B (zh) * | 2019-12-10 | 2023-09-15 | 上海航天控制技术研究所 | 基于卫星伪距/相对测量信息辅助的sins误差在线修正方法 |
CN111060140B (zh) * | 2019-12-31 | 2022-08-02 | 西北工业大学 | 一种地球椭球模型下的极区惯性导航误差获得方法 |
US11268813B2 (en) * | 2020-01-13 | 2022-03-08 | Honeywell International Inc. | Integrated inertial gravitational anomaly navigation system |
CN111829511A (zh) * | 2020-06-08 | 2020-10-27 | 中国航天空气动力技术研究院 | 一种基于m估计的auv组合导航方法及系统 |
CN112325841B (zh) * | 2020-10-26 | 2022-05-27 | 中国电子科技集团公司第五十四研究所 | 一种动中通天线安装误差角的估计方法 |
US11722903B2 (en) | 2021-04-09 | 2023-08-08 | Northrop Grumman Systems Corporation | Environmental verification for controlling access to data |
CN113310486B (zh) * | 2021-05-31 | 2023-03-21 | 武汉大学 | 一种万有引力定位方法及系统 |
CN116481564B (zh) * | 2023-03-11 | 2024-02-23 | 中国人民解放军国防科技大学 | 基于Psi角误差修正模型的极地双惯导协同标定方法 |
CN116734887B (zh) * | 2023-03-11 | 2024-01-30 | 中国人民解放军国防科技大学 | 基于速度误差修正模型的极地双惯导协同标定方法 |
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DE3438719A1 (de) | 1984-10-23 | 1986-04-24 | Bodenseewerk Gerätetechnik GmbH, 7770 Überlingen | Anordnung zur gegenseitigen lagebestimmung von mutter- und tochter-traegheitsnavigationssystemen |
US4874942A (en) * | 1987-10-26 | 1989-10-17 | Clauser John F | Rotation, acceleration, and gravity sensors using quantum-mechanical matter-wave interferometry with neutral atoms and molecules |
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JPH07239236A (ja) * | 1994-02-28 | 1995-09-12 | Hitachi Ltd | 移動体の状態量計測方法と装置および移動体の姿勢角演算装置 |
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-
2005
- 2005-03-23 US US11/087,902 patent/US7509216B2/en active Active
- 2005-03-24 CA CA2502340A patent/CA2502340C/en active Active
- 2005-03-29 EP EP10166098A patent/EP2259023B8/de active Active
- 2005-03-29 DE DE602005027773T patent/DE602005027773D1/de active Active
- 2005-03-29 EP EP05251937A patent/EP1582840B1/de active Active
- 2005-03-29 JP JP2005095365A patent/JP4989035B2/ja active Active
-
2009
- 2009-01-29 US US12/362,383 patent/US8311739B2/en active Active
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2782334C1 (ru) * | 2022-01-21 | 2022-10-25 | Акционерное общество "Инерциальные технологии "Технокомплекса" (АО "ИТТ") | Способ определения параметров ориентации объекта при помощи полуаналитической инерциальной навигационной системы с географической ориентацией осей четырехосной гироплатформы |
RU2798209C1 (ru) * | 2022-11-21 | 2023-06-19 | Акционерное общество "Государственное научно-производственное предприятие "Регион" (АО "ГНПП "Регион") | Способ автономной выставки бесплатформенной навигационной системы в процессе выхода управляемого объекта из пике после приводнения |
Also Published As
Publication number | Publication date |
---|---|
CA2502340C (en) | 2014-08-05 |
EP2259023B1 (de) | 2012-12-19 |
US8311739B2 (en) | 2012-11-13 |
US20090037107A1 (en) | 2009-02-05 |
EP2259023B8 (de) | 2013-02-13 |
EP1582840B1 (de) | 2011-05-04 |
US7509216B2 (en) | 2009-03-24 |
JP4989035B2 (ja) | 2012-08-01 |
EP1582840A1 (de) | 2005-10-05 |
JP2005283586A (ja) | 2005-10-13 |
EP2259023A1 (de) | 2010-12-08 |
CA2502340A1 (en) | 2005-09-29 |
US20090204323A1 (en) | 2009-08-13 |
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