DE602006002367D1 - Ität und kontinuität - Google Patents

Ität und kontinuität

Info

Publication number
DE602006002367D1
DE602006002367D1 DE602006002367T DE602006002367T DE602006002367D1 DE 602006002367 D1 DE602006002367 D1 DE 602006002367D1 DE 602006002367 T DE602006002367 T DE 602006002367T DE 602006002367 T DE602006002367 T DE 602006002367T DE 602006002367 D1 DE602006002367 D1 DE 602006002367D1
Authority
DE
Germany
Prior art keywords
satellite
calculates
pseudo
receiver
instantaneous
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
Application number
DE602006002367T
Other languages
English (en)
Inventor
Nicolas Martin
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.)
Thales SA
Original Assignee
Thales 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
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=34954333&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=DE602006002367(D1) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Thales SA filed Critical Thales SA
Publication of DE602006002367D1 publication Critical patent/DE602006002367D1/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • 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
    • G01S19/42—Determining position
    • G01S19/43—Determining position using carrier phase measurements, e.g. kinematic positioning; using long or short baseline interferometry
    • 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
    • G01S19/42—Determining position
    • G01S19/45—Determining position by combining measurements of signals from the satellite radio beacon positioning system with a supplementary measurement
    • G01S19/47—Determining position by combining measurements of signals from the satellite radio beacon positioning system with a supplementary measurement the supplementary measurement being an inertial measurement, e.g. tightly coupled inertial
DE602006002367T 2005-01-20 2006-01-03 Ität und kontinuität Active DE602006002367D1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0500592A FR2881008B1 (fr) 2005-01-20 2005-01-20 Recepteur de positionnement par satellite a integrite et continuite ameliorees
PCT/EP2006/050014 WO2006077174A1 (fr) 2005-01-20 2006-01-03 Recepteur de positionnement par satellite a integrite et continuite ameliorees

Publications (1)

Publication Number Publication Date
DE602006002367D1 true DE602006002367D1 (de) 2008-10-02

Family

ID=34954333

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602006002367T Active DE602006002367D1 (de) 2005-01-20 2006-01-03 Ität und kontinuität

Country Status (7)

Country Link
US (1) US7504996B2 (de)
EP (1) EP1839070B2 (de)
AT (1) ATE405852T1 (de)
CA (1) CA2589463C (de)
DE (1) DE602006002367D1 (de)
FR (1) FR2881008B1 (de)
WO (1) WO2006077174A1 (de)

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CN115485584A (zh) 2020-02-14 2022-12-16 斯威夫特导航股份有限公司 用于重新收敛gnss位置估计的系统和方法
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Also Published As

Publication number Publication date
EP1839070B1 (de) 2008-08-20
US7504996B2 (en) 2009-03-17
WO2006077174A1 (fr) 2006-07-27
FR2881008B1 (fr) 2007-04-20
US20080129586A1 (en) 2008-06-05
EP1839070B2 (de) 2014-04-30
EP1839070A1 (de) 2007-10-03
CA2589463A1 (fr) 2006-07-27
CA2589463C (fr) 2015-11-10
FR2881008A1 (fr) 2006-07-21
ATE405852T1 (de) 2008-09-15

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