FR2715724B1 - Procédé pour déterminer la position d'un avion à partir de données d'accélération d'un système inertiel ainsi qu'à partir de données de sortie d'un système de navigation, et dispositif. - Google Patents

Procédé pour déterminer la position d'un avion à partir de données d'accélération d'un système inertiel ainsi qu'à partir de données de sortie d'un système de navigation, et dispositif.

Info

Publication number
FR2715724B1
FR2715724B1 FR9501224A FR9501224A FR2715724B1 FR 2715724 B1 FR2715724 B1 FR 2715724B1 FR 9501224 A FR9501224 A FR 9501224A FR 9501224 A FR9501224 A FR 9501224A FR 2715724 B1 FR2715724 B1 FR 2715724B1
Authority
FR
France
Prior art keywords
airplane
determining
well
output data
navigation system
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.)
Expired - Fee Related
Application number
FR9501224A
Other languages
English (en)
Other versions
FR2715724A1 (fr
Inventor
Stefan Buckreub
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.)
Deutsches Zentrum fuer Luft und Raumfahrt eV
Original Assignee
Deutsche Forschungs und Versuchsanstalt fuer Luft und Raumfahrt eV DFVLR
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 Deutsche Forschungs und Versuchsanstalt fuer Luft und Raumfahrt eV DFVLR filed Critical Deutsche Forschungs und Versuchsanstalt fuer Luft und Raumfahrt eV DFVLR
Publication of FR2715724A1 publication Critical patent/FR2715724A1/fr
Application granted granted Critical
Publication of FR2715724B1 publication Critical patent/FR2715724B1/fr
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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
    • 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
    • G01C21/165—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 combined with non-inertial navigation instruments
    • G01C21/1652—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 combined with non-inertial navigation instruments with ranging devices, e.g. LIDAR or RADAR
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S19/00—Satellite radio beacon positioning systems; Determining position, velocity or attitude using signals transmitted by such systems
    • G01S19/38—Determining a navigation solution using signals transmitted by a satellite radio beacon positioning system
    • G01S19/39—Determining a navigation solution using signals transmitted by a satellite radio beacon positioning system the satellite radio beacon positioning system transmitting time-stamped messages, e.g. GPS [Global Positioning System], GLONASS [Global Orbiting Navigation Satellite System] or GALILEO
    • G01S19/40—Correcting position, velocity or attitude
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S13/00—Systems using the reflection or reradiation of radio waves, e.g. radar systems; Analogous systems using reflection or reradiation of waves whose nature or wavelength is irrelevant or unspecified
    • G01S13/02—Systems using reflection of radio waves, e.g. primary radar systems; Analogous systems
    • G01S13/50—Systems of measurement based on relative movement of target
    • G01S13/58—Velocity or trajectory determination systems; Sense-of-movement determination systems
    • G01S13/60—Velocity or trajectory determination systems; Sense-of-movement determination systems wherein the transmitter and receiver are mounted on the moving object, e.g. for determining ground speed, drift angle, ground track
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S13/00—Systems using the reflection or reradiation of radio waves, e.g. radar systems; Analogous systems using reflection or reradiation of waves whose nature or wavelength is irrelevant or unspecified
    • G01S13/86—Combinations of radar systems with non-radar systems, e.g. sonar, direction finder
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S13/00—Systems using the reflection or reradiation of radio waves, e.g. radar systems; Analogous systems using reflection or reradiation of waves whose nature or wavelength is irrelevant or unspecified
    • G01S13/88—Radar or analogous systems specially adapted for specific applications
    • G01S13/89—Radar or analogous systems specially adapted for specific applications for mapping or imaging
    • G01S13/90—Radar or analogous systems specially adapted for specific applications for mapping or imaging using synthetic aperture techniques, e.g. synthetic aperture radar [SAR] techniques

Landscapes

  • Engineering & Computer Science (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • Navigation (AREA)
  • Radar Systems Or Details Thereof (AREA)
FR9501224A 1994-02-02 1995-02-02 Procédé pour déterminer la position d'un avion à partir de données d'accélération d'un système inertiel ainsi qu'à partir de données de sortie d'un système de navigation, et dispositif. Expired - Fee Related FR2715724B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE4403190A DE4403190C1 (de) 1994-02-02 1994-02-02 Verfahren zum Bestimmen der Position eines Flugzeugs aus Beschleunigungsdaten eines Inertialsystems sowie aus Ausgabedaten eines Navigationssystems und Einrichtung zur Durchführung des Verfahrens

Publications (2)

Publication Number Publication Date
FR2715724A1 FR2715724A1 (fr) 1995-08-04
FR2715724B1 true FR2715724B1 (fr) 1998-01-30

Family

ID=6509310

Family Applications (1)

Application Number Title Priority Date Filing Date
FR9501224A Expired - Fee Related FR2715724B1 (fr) 1994-02-02 1995-02-02 Procédé pour déterminer la position d'un avion à partir de données d'accélération d'un système inertiel ainsi qu'à partir de données de sortie d'un système de navigation, et dispositif.

Country Status (3)

Country Link
US (1) US5590044A (fr)
DE (1) DE4403190C1 (fr)
FR (1) FR2715724B1 (fr)

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US5941935A (en) * 1996-09-23 1999-08-24 Fernandez; Manuel Azimuth-axis drift rate determination in an inertial navigator
DE19714985A1 (de) * 1997-04-10 1998-10-22 Litef Gmbh Verfahren zur Überprüfung der Zuverlässigkeit von nominellen Positionsbestimmungen
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US6082666A (en) * 1997-12-03 2000-07-04 Raytheon Company System for accurately determining missile vertical velocity and altitude
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US6204806B1 (en) * 1999-02-26 2001-03-20 Rockwell Collins, Inc. Method of enhancing receiver autonomous GPS navigation integrity monitoring and GPS receiver implementing the same
US8446321B2 (en) 1999-03-05 2013-05-21 Omnipol A.S. Deployable intelligence and tracking system for homeland security and search and rescue
US7908077B2 (en) 2003-06-10 2011-03-15 Itt Manufacturing Enterprises, Inc. Land use compatibility planning software
US7739167B2 (en) 1999-03-05 2010-06-15 Era Systems Corporation Automated management of airport revenues
US7570214B2 (en) 1999-03-05 2009-08-04 Era Systems, Inc. Method and apparatus for ADS-B validation, active and passive multilateration, and elliptical surviellance
US7889133B2 (en) 1999-03-05 2011-02-15 Itt Manufacturing Enterprises, Inc. Multilateration enhancements for noise and operations management
US8203486B1 (en) 1999-03-05 2012-06-19 Omnipol A.S. Transmitter independent techniques to extend the performance of passive coherent location
US7777675B2 (en) 1999-03-05 2010-08-17 Era Systems Corporation Deployable passive broadband aircraft tracking
US7782256B2 (en) 1999-03-05 2010-08-24 Era Systems Corporation Enhanced passive coherent location techniques to track and identify UAVs, UCAVs, MAVs, and other objects
US7612716B2 (en) 1999-03-05 2009-11-03 Era Systems Corporation Correlation of flight track data with other data sources
US7667647B2 (en) 1999-03-05 2010-02-23 Era Systems Corporation Extension of aircraft tracking and positive identification from movement areas into non-movement areas
GB9906781D0 (en) 1999-03-24 1999-05-19 British Aerospace Height estimating apparatus
US6462703B2 (en) * 2000-07-27 2002-10-08 Innovative Solutions & Support, Inc. Method and system for high precision altitude measurement over hostile terrain
US6831599B2 (en) * 2002-08-26 2004-12-14 Honeywell International Inc. Remote velocity sensor slaved to an integrated GPS/INS
JP2004271233A (ja) * 2003-03-05 2004-09-30 Fujitsu Ten Ltd 異常検出機能を備えたレーダ装置
DE10338234A1 (de) * 2003-08-14 2004-09-23 Siemens Ag Verfahren zur Ortung eines bewegten Objekts
JP4819802B2 (ja) * 2004-05-12 2011-11-24 ノースロップ グラマン システムズ コーポレーション 複数のナビゲーションコンポーネントの整合システム及び方法
CN1314945C (zh) * 2005-11-04 2007-05-09 北京航空航天大学 一种sins/gps组合导航系统的空中机动对准方法
US8666661B2 (en) * 2006-03-31 2014-03-04 The Boeing Company Video navigation
US7965227B2 (en) 2006-05-08 2011-06-21 Era Systems, Inc. Aircraft tracking using low cost tagging as a discriminator
US7328104B2 (en) * 2006-05-17 2008-02-05 Honeywell International Inc. Systems and methods for improved inertial navigation
DE102007030987A1 (de) * 2007-07-04 2009-01-08 Robert Bosch Gmbh Vorrichtung zur Bestimmung einer Geschwindigkeit mit einem Beschleunigungssensor
DE102008019621A1 (de) * 2008-02-29 2009-09-03 Symeo Gmbh Messvorrichtung und Messverfahren zur Bestimmung eines Abstands, einer Geschwindigkeit, einer Beschleunigung, eines Rucks, eines Eingangswinkels, einer Eingangswinkelgeschwindigkeit, einer Eingangswinkelbeschleunigung, und/oder eines Eingangswinkelrucks zwischen einer Sende- und Empfangseinrichtung und einem Objekt
LU92541B1 (en) * 2014-09-10 2016-03-11 Iee Sarl Radar sensing of vehicle occupancy
US9939524B2 (en) 2015-02-04 2018-04-10 Honeywell International Inc. Systems and methods for measuring velocity with a radar altimeter
US9550583B2 (en) 2015-03-03 2017-01-24 Honeywell International Inc. Aircraft LRU data collection and reliability prediction
CN104820758A (zh) * 2015-05-20 2015-08-05 江苏华豪航海电器有限公司 一种基于奇异值分解的传递对准精度评估可观测性分析方法
WO2017084045A1 (fr) * 2015-11-18 2017-05-26 深圳市大疆创新科技有限公司 Aéronef véhicule aérien sans pilote ainsi que procédé et système de navigation
US10641885B2 (en) 2017-07-21 2020-05-05 Honeywell International Inc. Systems and methods for measuring velocity and acceleration with a radar altimeter
CN111678538B (zh) * 2020-07-29 2023-06-09 中国电子科技集团公司第二十六研究所 一种基于速度匹配的动态水平仪误差补偿方法
DE102020131669B3 (de) * 2020-11-30 2021-12-23 Daimler Ag Verfahren zur Erkennung von Fehlfunktionen in Inertialmesseinheiten

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Also Published As

Publication number Publication date
FR2715724A1 (fr) 1995-08-04
DE4403190C1 (de) 1995-07-27
US5590044A (en) 1996-12-31

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