ZA200106724B - Device for hybridizing a satellite positioning receiver with an inertial unit. - Google Patents

Device for hybridizing a satellite positioning receiver with an inertial unit. Download PDF

Info

Publication number
ZA200106724B
ZA200106724B ZA200106724A ZA200106724A ZA200106724B ZA 200106724 B ZA200106724 B ZA 200106724B ZA 200106724 A ZA200106724 A ZA 200106724A ZA 200106724 A ZA200106724 A ZA 200106724A ZA 200106724 B ZA200106724 B ZA 200106724B
Authority
ZA
South Africa
Prior art keywords
vector
satellite
craft
pseudo
navigation computer
Prior art date
Application number
ZA200106724A
Other languages
English (en)
Inventor
Nicolas Martin
Original Assignee
Thales Avionics Sa
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 Thales Avionics Sa filed Critical Thales Avionics Sa
Publication of ZA200106724B publication Critical patent/ZA200106724B/en

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO 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
    • G01S19/00Satellite radio beacon positioning systems; Determining position, velocity or attitude using signals transmitted by such systems
    • G01S19/38Determining a navigation solution using signals transmitted by a satellite radio beacon positioning system
    • G01S19/39Determining 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
    • G01S19/42Determining position
    • G01S19/48Determining position by combining or switching between position solutions derived from the satellite radio beacon positioning system and position solutions derived from a further system
    • G01S19/49Determining position by combining or switching between position solutions derived from the satellite radio beacon positioning system and position solutions derived from a further system whereby the further system is an inertial position system, e.g. loosely-coupled
    • 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
    • G01C21/165Navigation; 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
    • 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
    • G01C21/165Navigation; 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
    • G01C21/1652Navigation; 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

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)
  • Position Fixing By Use Of Radio Waves (AREA)
ZA200106724A 1999-12-21 2001-08-15 Device for hybridizing a satellite positioning receiver with an inertial unit. ZA200106724B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9916164A FR2802732B1 (fr) 1999-12-21 1999-12-21 Dispositif d'hybridation d'un recepteur de positionnement par satellites avec une centrale inertielle

Publications (1)

Publication Number Publication Date
ZA200106724B true ZA200106724B (en) 2002-02-15

Family

ID=9553558

Family Applications (1)

Application Number Title Priority Date Filing Date
ZA200106724A ZA200106724B (en) 1999-12-21 2001-08-15 Device for hybridizing a satellite positioning receiver with an inertial unit.

Country Status (5)

Country Link
EP (1) EP1157284A1 (de)
FR (1) FR2802732B1 (de)
IL (2) IL144914A0 (de)
WO (1) WO2001046712A1 (de)
ZA (1) ZA200106724B (de)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2866423B1 (fr) * 2004-02-13 2006-05-05 Thales Sa Dispositif de surveillance de l'integrite des informations delivrees par un systeme hybride ins/gnss
FR2895073B1 (fr) 2005-12-20 2008-02-08 Thales Sa Dispositif d'hybridation en boucle fermee avec surveillance de l'integrite des mesures.
CN104913781A (zh) * 2015-06-04 2015-09-16 南京航空航天大学 一种基于动态信息分配的非等间隔联邦滤波方法
CN110954092B (zh) * 2019-11-28 2023-09-15 上海航天控制技术研究所 基于相对测量信息辅助的协同导航方法
CN113048989B (zh) * 2021-04-06 2022-12-09 北京三快在线科技有限公司 一种无人驾驶设备的定位方法及定位装置
FR3138693A1 (fr) 2022-08-04 2024-02-09 Gaztransport Et Technigaz Procédé et système de correction de données émises par des capteurs pour l'optimisation de navigation de navire

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5583774A (en) * 1994-06-16 1996-12-10 Litton Systems, Inc. Assured-integrity monitored-extrapolation navigation apparatus
US5787384A (en) * 1995-11-22 1998-07-28 E-Systems, Inc. Apparatus and method for determining velocity of a platform

Also Published As

Publication number Publication date
FR2802732A1 (fr) 2001-06-22
WO2001046712A1 (fr) 2001-06-28
EP1157284A1 (de) 2001-11-28
IL144914A (en) 2006-06-11
FR2802732B1 (fr) 2002-03-22
IL144914A0 (en) 2002-06-30

Similar Documents

Publication Publication Date Title
CN113819906B (zh) 一种基于统计相似度量的组合导航鲁棒滤波方法
US5757316A (en) Attitude determination utilizing an inertial measurement unit and a plurality of satellite transmitters
US6424914B1 (en) Fully-coupled vehicle positioning method and system thereof
US6831599B2 (en) Remote velocity sensor slaved to an integrated GPS/INS
US5787384A (en) Apparatus and method for determining velocity of a platform
EP0965048B1 (de) Kontinuierliche genauigkeitsverbesserung für zivile gps-empfänger
CN111965685B (zh) 一种基于多普勒信息的低轨卫星/惯性组合导航定位方法
CN109471146B (zh) 一种基于ls-svm的自适应容错gps/ins组合导航方法
US20100179758A1 (en) Aircraft navigation using the global positioning system and an attitude and heading reference system
CA2384965A1 (en) Solution separation method and apparatus for ground-augmented global positioning system
EP0986733B1 (de) Robuste gps-zeitreferenze für raumfahrtanwendung
CA2721257A1 (en) Satellite-based positioning receiver
JP2001183439A (ja) 統計的フィルタの使用に基づいた汎用位置決めシステム
JP5007467B2 (ja) 編隊を組む宇宙船グループ内の一宇宙船用の、2周波数信号を解析することによる相対位置制御装置
WO2008097346A2 (en) Method for fusing multiple gps measurement types into a weighted least squares solution
van Graas et al. High‐Accuracy Differential Positioning for Satellite‐Based Systems Without Using Code‐Phase Measurements 1
JP2001507797A (ja) Gps受信機の障害検出の方法およびシステム
WO1998025108A1 (en) A neural network-based system for improving the accuracy of global positioning system signals
CN115327588A (zh) 一种基于网络rtk的无人自动化作业特种车高精度定位方法
ZA200106724B (en) Device for hybridizing a satellite positioning receiver with an inertial unit.
CN115356754A (zh) 一种基于gnss和低轨卫星的组合导航定位方法
CN110988932B (zh) 一种提高星载gps接收机实时钟差解算精度的方法
CN116878498A (zh) 一种多频bds/ins组合空中加油相对导航系统和方法
CN116105729A (zh) 一种针对野外洞穴森林环境侦察的多传感器融合定位方法
Hutton et al. 10 years of direct georeferencing for airborne photogrammetry