CA2384965A1 - Solution separation method and apparatus for ground-augmented global positioning system - Google Patents
Solution separation method and apparatus for ground-augmented global positioning system Download PDFInfo
- Publication number
- CA2384965A1 CA2384965A1 CA002384965A CA2384965A CA2384965A1 CA 2384965 A1 CA2384965 A1 CA 2384965A1 CA 002384965 A CA002384965 A CA 002384965A CA 2384965 A CA2384965 A CA 2384965A CA 2384965 A1 CA2384965 A1 CA 2384965A1
- Authority
- CA
- Canada
- Prior art keywords
- determining
- solution
- vehicle
- subsolution
- pseudoranges
- 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.)
- Abandoned
Links
- 238000000926 separation method Methods 0.000 title claims abstract description 40
- 238000012937 correction Methods 0.000 claims abstract description 127
- 238000000034 method Methods 0.000 claims abstract description 34
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- 238000012544 monitoring process Methods 0.000 claims description 3
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- 238000004364 calculation method Methods 0.000 abstract description 5
- 239000013598 vector Substances 0.000 description 61
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- 239000011159 matrix material Substances 0.000 description 14
- 238000009499 grossing Methods 0.000 description 9
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- 238000001514 detection method Methods 0.000 description 7
- 230000005484 gravity Effects 0.000 description 7
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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
- G01S19/01—Satellite radio beacon positioning systems transmitting time-stamped messages, e.g. GPS [Global Positioning System], GLONASS [Global Orbiting Navigation Satellite System] or GALILEO
- G01S19/13—Receivers
- G01S19/14—Receivers specially adapted for specific applications
- G01S19/15—Aircraft landing systems
-
- 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
- G01S19/01—Satellite radio beacon positioning systems transmitting time-stamped messages, e.g. GPS [Global Positioning System], GLONASS [Global Orbiting Navigation Satellite System] or GALILEO
- G01S19/03—Cooperating elements; Interaction or communication between different cooperating elements or between cooperating elements and receivers
- G01S19/07—Cooperating elements; Interaction or communication between different cooperating elements or between cooperating elements and receivers providing data for correcting measured positioning data, e.g. DGPS [differential GPS] or ionosphere corrections
- G01S19/071—DGPS corrections
-
- 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
- G01S19/01—Satellite radio beacon positioning systems transmitting time-stamped messages, e.g. GPS [Global Positioning System], GLONASS [Global Orbiting Navigation Satellite System] or GALILEO
- G01S19/03—Cooperating elements; Interaction or communication between different cooperating elements or between cooperating elements and receivers
- G01S19/07—Cooperating elements; Interaction or communication between different cooperating elements or between cooperating elements and receivers providing data for correcting measured positioning data, e.g. DGPS [differential GPS] or ionosphere corrections
- G01S19/073—Cooperating elements; Interaction or communication between different cooperating elements or between cooperating elements and receivers providing data for correcting measured positioning data, e.g. DGPS [differential GPS] or ionosphere corrections involving a network of fixed stations
- G01S19/074—Cooperating elements; Interaction or communication between different cooperating elements or between cooperating elements and receivers providing data for correcting measured positioning data, e.g. DGPS [differential GPS] or ionosphere corrections involving a network of fixed stations providing integrity data, e.g. WAAS
-
- 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
- G01S19/41—Differential correction, e.g. DGPS [differential GPS]
-
- 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
- G01S5/00—Position-fixing by co-ordinating two or more direction or position line determinations; Position-fixing by co-ordinating two or more distance determinations
- G01S5/0009—Transmission of position information to remote stations
- G01S5/009—Transmission of differential positioning data to mobile
-
- 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
- G01S19/01—Satellite radio beacon positioning systems transmitting time-stamped messages, e.g. GPS [Global Positioning System], GLONASS [Global Orbiting Navigation Satellite System] or GALILEO
- G01S19/13—Receivers
- G01S19/20—Integrity monitoring, fault detection or fault isolation of space segment
Landscapes
- Engineering & Computer Science (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Computer Networks & Wireless Communication (AREA)
- Aviation & Aerospace Engineering (AREA)
- Computer Security & Cryptography (AREA)
- Position Fixing By Use Of Radio Waves (AREA)
- Navigation (AREA)
- Geophysics And Detection Of Objects (AREA)
- Consolidation Of Soil By Introduction Of Solidifying Substances Into Soil (AREA)
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US09/396,193 US6760663B2 (en) | 1999-09-14 | 1999-09-14 | Solution separation method and apparatus for ground-augmented global positioning system |
| US09/396,193 | 1999-09-14 | ||
| PCT/US2000/025274 WO2001020360A1 (en) | 1999-09-14 | 2000-09-14 | Solution separation method and apparatus for ground-augmented global positioning system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CA2384965A1 true CA2384965A1 (en) | 2001-03-22 |
Family
ID=23566245
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CA002384965A Abandoned CA2384965A1 (en) | 1999-09-14 | 2000-09-14 | Solution separation method and apparatus for ground-augmented global positioning system |
Country Status (7)
| Country | Link |
|---|---|
| US (1) | US6760663B2 (enExample) |
| EP (1) | EP1212634B1 (enExample) |
| JP (1) | JP5019687B2 (enExample) |
| AT (1) | ATE390638T1 (enExample) |
| CA (1) | CA2384965A1 (enExample) |
| DE (1) | DE60038453T2 (enExample) |
| WO (1) | WO2001020360A1 (enExample) |
Families Citing this family (41)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6985812B2 (en) | 2001-04-13 | 2006-01-10 | General Dynamics Advanced Information Systems, Inc. | System and method for detecting interference in global positioning satellite signals |
| US7512492B2 (en) * | 2001-04-13 | 2009-03-31 | General Dynamics Advanced Information Systems, Inc. | System and method for detecting interference in global positioning satellite signals |
| US6549829B1 (en) * | 2001-10-31 | 2003-04-15 | The Boeing Company | Skipping filter for inertially augmented landing system |
| US6809683B2 (en) * | 2002-11-18 | 2004-10-26 | Honeywell International Inc. | Portable tester for LAAS ground facility |
| US6904377B2 (en) * | 2003-03-17 | 2005-06-07 | Northrop Grumman Corporation | Method for measuring force-dependent gyroscope sensitivity |
| RU2258940C1 (ru) * | 2003-12-31 | 2005-08-20 | Военно-космическая академия им. А.Ф. Можайского | Спутниковая система для определения местоположения судов и самолетов, потерпевших аварию |
| US20060234641A1 (en) * | 2005-02-03 | 2006-10-19 | Lucent Technologies Inc. | System for using an existing cellular network to detect incidents of GPS jaming |
| US7593811B2 (en) * | 2005-03-31 | 2009-09-22 | Deere & Company | Method and system for following a lead vehicle |
| US7479922B2 (en) * | 2005-03-31 | 2009-01-20 | Deere & Company | Method and system for determining the location of a vehicle |
| US7720598B2 (en) | 2005-03-31 | 2010-05-18 | Deere & Company | System and method for determining a position of a vehicle with compensation for noise or measurement error |
| US7647177B2 (en) * | 2005-03-31 | 2010-01-12 | Deere & Company | System and method for determining a position of a vehicle |
| US7653483B2 (en) | 2005-03-31 | 2010-01-26 | Deere & Company | System and method for determining a position of a vehicle |
| US7609204B2 (en) * | 2005-08-30 | 2009-10-27 | Honeywell International Inc. | System and method for dynamically estimating output variances for carrier-smoothing filters |
| FR2896073B1 (fr) * | 2006-01-11 | 2008-02-08 | Airbus France Sas | Systeme de pilotage d'un aeronef, au moins pour piloter l'aeronef lors d'une approche autonome en vue d'un atterrissage. |
| DE102006003308A1 (de) * | 2006-01-23 | 2007-07-26 | Eads Astrium Gmbh | Verfahren und Vorrichtung zur Bestimmung von Protection-Levels für Satellitennavigationssysteme |
| FR2906894B1 (fr) * | 2006-10-09 | 2013-09-06 | Sagem Defense Securite | Procede de localisation d'un vehicule par satellites et garantie d'integrite avec selection d'un sous-groupe de satellites |
| US8014948B2 (en) * | 2007-12-07 | 2011-09-06 | Honeywell International Inc. | Navigation system with apparatus for detecting accuracy failures |
| US20090182493A1 (en) * | 2008-01-15 | 2009-07-16 | Honeywell International, Inc. | Navigation system with apparatus for detecting accuracy failures |
| US20090182494A1 (en) * | 2008-01-15 | 2009-07-16 | Honeywell International, Inc. | Navigation system with apparatus for detecting accuracy failures |
| US20090182495A1 (en) * | 2008-01-15 | 2009-07-16 | Honeywell International, Inc. | Navigation system with apparatus for detecting accuracy failures |
| US8600671B2 (en) * | 2008-04-04 | 2013-12-03 | The Boeing Company | Low authority GPS aiding of navigation system for anti-spoofing |
| FR2949852B1 (fr) * | 2009-09-07 | 2011-12-16 | Sagem Defense Securite | Procede et systeme de determination de limites de protection avec extrapolation integre sur un horizon temporel donne |
| US8976064B2 (en) * | 2012-09-06 | 2015-03-10 | Honeywell International Inc. | Systems and methods for solution separation for ground-augmented multi-constellation terminal area navigation and precision approach guidance |
| US9341718B2 (en) | 2012-09-07 | 2016-05-17 | Honeywell International Inc. | Method and system for providing integrity for hybrid attitude and true heading |
| US8898011B2 (en) * | 2012-09-12 | 2014-11-25 | Raytheon Company | Method for maintaining integrity against erroneous ephemeris for a differential GPS based navigation solution supporting fast system startup |
| FR3002032B1 (fr) * | 2013-02-08 | 2016-02-12 | Dassault Aviat | Systeme et procede d'aide a la navigation d'un aeronef |
| US9547086B2 (en) * | 2013-03-26 | 2017-01-17 | Honeywell International Inc. | Selected aspects of advanced receiver autonomous integrity monitoring application to kalman filter based navigation filter |
| US9488732B1 (en) * | 2013-07-24 | 2016-11-08 | Rockwell Collins, Inc. | GPS optimization for limited data |
| CN104749582B (zh) * | 2013-12-27 | 2017-11-21 | 中国移动通信集团公司 | 差分数据的发送方法、gps定位数据的确定方法及装置 |
| US9746562B2 (en) | 2014-06-30 | 2017-08-29 | The Boeing Company | Portable ground based augmentation system |
| US9939532B2 (en) | 2015-01-09 | 2018-04-10 | Honeywell International Inc. | Heading for a hybrid navigation solution based on magnetically calibrated measurements |
| EP3264343A1 (en) * | 2016-06-30 | 2018-01-03 | Honeywell International Inc. | Devices, methods, and systems for airside performance analysis |
| US10955261B2 (en) * | 2017-04-17 | 2021-03-23 | Rosemount Aerospace Inc. | Air data attitude reference system |
| US10284326B2 (en) * | 2017-05-10 | 2019-05-07 | Talen-X, Inc. | Penalty-based environment monitoring |
| US11662472B2 (en) * | 2020-04-20 | 2023-05-30 | Honeywell International Inc. | Integrity monitoring of odometry measurements within a navigation system |
| US11892544B2 (en) | 2020-05-01 | 2024-02-06 | Honeywell International Inc. | GNSS data integrity monitoring as a connected service |
| CN111913203B (zh) * | 2020-07-08 | 2023-01-10 | 北京航空航天大学 | 一种动态基线定位域监测方法 |
| DE102020119803A1 (de) * | 2020-07-28 | 2022-02-03 | Airbus Defence and Space GmbH | Präzisionsanflug- und Landesystem für Luftfahrzeuge |
| CN112526549B (zh) * | 2020-12-01 | 2022-03-15 | 北京航空航天大学 | 一种地基增强系统完好性故障识别方法及系统 |
| US12153148B2 (en) * | 2021-05-17 | 2024-11-26 | Reliable Robotics Corporation | Radar altimeter augmented receiver autonomous integrity monitoring in aircraft |
| US12442936B2 (en) | 2021-06-14 | 2025-10-14 | Honeywell International Inc. | Inertial coasting position and velocity solution separation |
Family Cites Families (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5216611A (en) * | 1991-02-08 | 1993-06-01 | Rockwell International Corporation | Integrated enroute and approach guidance system for aircraft |
| JPH08297158A (ja) * | 1995-04-26 | 1996-11-12 | Furuno Electric Co Ltd | 測位装置および測位用衛星の異常検知方法 |
| US5600329A (en) * | 1995-06-30 | 1997-02-04 | Honeywell Inc. | Differential satellite positioning system ground station with integrity monitoring |
| US5884220A (en) | 1996-07-16 | 1999-03-16 | Trimble Navigation Limited | Method and apparatus to improve overall performance of a DGPS receiver |
| US5760737A (en) * | 1996-09-11 | 1998-06-02 | Honeywell Inc. | Navigation system with solution separation apparatus for detecting accuracy failures |
| US5786773A (en) | 1996-10-02 | 1998-07-28 | The Boeing Company | Local-area augmentation system for satellite navigation precision-approach system |
| JP3545640B2 (ja) * | 1999-04-30 | 2004-07-21 | 株式会社東芝 | ローカルエリア統合測位システム |
-
1999
- 1999-09-14 US US09/396,193 patent/US6760663B2/en not_active Expired - Lifetime
-
2000
- 2000-09-14 AT AT00970456T patent/ATE390638T1/de not_active IP Right Cessation
- 2000-09-14 EP EP00970456A patent/EP1212634B1/en not_active Expired - Lifetime
- 2000-09-14 JP JP2001523891A patent/JP5019687B2/ja not_active Expired - Lifetime
- 2000-09-14 CA CA002384965A patent/CA2384965A1/en not_active Abandoned
- 2000-09-14 WO PCT/US2000/025274 patent/WO2001020360A1/en not_active Ceased
- 2000-09-14 DE DE60038453T patent/DE60038453T2/de not_active Expired - Lifetime
Also Published As
| Publication number | Publication date |
|---|---|
| ATE390638T1 (de) | 2008-04-15 |
| JP2003509697A (ja) | 2003-03-11 |
| DE60038453D1 (de) | 2008-05-08 |
| US20010020214A1 (en) | 2001-09-06 |
| EP1212634B1 (en) | 2008-03-26 |
| DE60038453T2 (de) | 2009-08-27 |
| WO2001020360A9 (en) | 2002-09-26 |
| US6760663B2 (en) | 2004-07-06 |
| EP1212634A1 (en) | 2002-06-12 |
| WO2001020360A1 (en) | 2001-03-22 |
| JP5019687B2 (ja) | 2012-09-05 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| FZDE | Discontinued |