WO2007086899A3 - Transponder landing system augmentation of the global positioning system - Google Patents
Transponder landing system augmentation of the global positioning system Download PDFInfo
- Publication number
- WO2007086899A3 WO2007086899A3 PCT/US2006/012633 US2006012633W WO2007086899A3 WO 2007086899 A3 WO2007086899 A3 WO 2007086899A3 US 2006012633 W US2006012633 W US 2006012633W WO 2007086899 A3 WO2007086899 A3 WO 2007086899A3
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- aircraft
- ground station
- navigation system
- gps navigation
- transponder
- Prior art date
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
- G01S19/01—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
- G01S19/13—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
- G01S19/073—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
- G01S19/01—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
- G01S19/23—Testing, monitoring, correcting or calibrating of receiver elements
-
- 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
- G01S5/02—Position-fixing by co-ordinating two or more direction or position line determinations; Position-fixing by co-ordinating two or more distance determinations using radio waves
- G01S5/06—Position of source determined by co-ordinating a plurality of position lines defined by path-difference measurements
Abstract
A GPS navigation system augmentation using a transponder landing system. Initially, the position of a reference ground station is determined. When an aircraft using an on-board GPS navigation system approaches the ground station, the ground station accurately determines the position of the aircraft using the aircraft's transponder replies. In addition, the ground station receives a current position for the aircraft measured by an on-board GPS navigation system. By comparing the position of the aircraft determined from the transponder replies with the GPS- calculated position provided by the aircraft, the ground station determine error information for the on-board GPS navigation system. The ground station then transmits the error information back to the aircraft. Using this error information, the on-board GPS navigation system can improve the accuracy of future position calculations for the aircraft.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US66651005P | 2005-03-29 | 2005-03-29 | |
US60/666,510 | 2005-03-29 |
Publications (2)
Publication Number | Publication Date |
---|---|
WO2007086899A2 WO2007086899A2 (en) | 2007-08-02 |
WO2007086899A3 true WO2007086899A3 (en) | 2007-11-15 |
Family
ID=38309648
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/US2006/012633 WO2007086899A2 (en) | 2005-03-29 | 2006-03-29 | Transponder landing system augmentation of the global positioning system |
Country Status (1)
Country | Link |
---|---|
WO (1) | WO2007086899A2 (en) |
Families Citing this family (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7739167B2 (en) | 1999-03-05 | 2010-06-15 | Era Systems Corporation | Automated management of airport revenues |
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 |
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 |
US8203486B1 (en) | 1999-03-05 | 2012-06-19 | Omnipol A.S. | Transmitter independent techniques to extend the performance of passive coherent location |
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 |
US7777675B2 (en) | 1999-03-05 | 2010-08-17 | Era Systems Corporation | Deployable passive broadband aircraft tracking |
US7889133B2 (en) | 1999-03-05 | 2011-02-15 | Itt Manufacturing Enterprises, Inc. | Multilateration enhancements for noise and operations management |
US7908077B2 (en) | 2003-06-10 | 2011-03-15 | Itt Manufacturing Enterprises, Inc. | Land use compatibility planning software |
US8446321B2 (en) | 1999-03-05 | 2013-05-21 | Omnipol A.S. | Deployable intelligence and tracking system for homeland security and search and rescue |
FR2898672B1 (en) * | 2006-03-14 | 2009-07-03 | Thales Sa | METHOD FOR AIDING NAVIGATION OF AN AIRCRAFT WITH FLIGHT PLAN UPDATE |
US7965227B2 (en) | 2006-05-08 | 2011-06-21 | Era Systems, Inc. | Aircraft tracking using low cost tagging as a discriminator |
CN100424522C (en) * | 2007-09-26 | 2008-10-08 | 北京航空航天大学 | Device and method used for layout satellite navigation foundation region reinforced system |
FR2927455B1 (en) * | 2008-02-08 | 2014-03-21 | Thales Sa | METHODS OF OPTIMIZING THE LOCALIZATION OF AN AIRCRAFT ON THE SOIL AND IN TAKE-OFF AND LANDING PHASES |
CN102520606B (en) * | 2011-11-15 | 2013-07-10 | 上海卫星工程研究所 | Aircraft system clock time correcting and redundancy correction method |
US9476985B2 (en) * | 2013-03-20 | 2016-10-25 | Honeywell International Inc. | System and method for real time subset geometry screening satellite constellations |
EP2894622A1 (en) * | 2014-01-10 | 2015-07-15 | Teia Limited | Precision guidance method and system for aircraft approaching and landing |
US10281586B2 (en) | 2016-04-07 | 2019-05-07 | Thales USA, Inc. | Transmission data for flight check |
JP6288745B1 (en) * | 2017-04-07 | 2018-03-07 | 国立研究開発法人 海上・港湾・航空技術研究所 | Method and apparatus for estimating the navigation performance of an aircraft having a function of performing navigation using GNSS, as well as a method for detecting deterioration of aircraft's aviation performance and an apparatus for monitoring aircraft navigation performance |
CN108415027B (en) * | 2018-02-26 | 2021-09-07 | 中国科学院上海光学精密机械研究所 | Active navigation positioning device and navigation positioning method for aircraft |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3665464A (en) * | 1969-05-01 | 1972-05-23 | Goodyear Aerospace Corp | Method and apparatus for high speed vehicle position acquisition |
US5017930A (en) * | 1990-01-25 | 1991-05-21 | John R. Stoltz | Precision landing system |
EP0498655B1 (en) * | 1991-02-08 | 1996-08-28 | Rockwell International Corporation | Integrated enroute and approach guidance system for aircraft |
US5786773A (en) * | 1996-10-02 | 1998-07-28 | The Boeing Company | Local-area augmentation system for satellite navigation precision-approach system |
EP1010988A2 (en) * | 1998-12-10 | 2000-06-21 | Hughes Electronics Corporation | Method and system for incorporating two-way ranging navigation as a calibration reference for GPS |
-
2006
- 2006-03-29 WO PCT/US2006/012633 patent/WO2007086899A2/en active Application Filing
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3665464A (en) * | 1969-05-01 | 1972-05-23 | Goodyear Aerospace Corp | Method and apparatus for high speed vehicle position acquisition |
US5017930A (en) * | 1990-01-25 | 1991-05-21 | John R. Stoltz | Precision landing system |
EP0498655B1 (en) * | 1991-02-08 | 1996-08-28 | Rockwell International Corporation | Integrated enroute and approach guidance system for aircraft |
US5786773A (en) * | 1996-10-02 | 1998-07-28 | The Boeing Company | Local-area augmentation system for satellite navigation precision-approach system |
EP1010988A2 (en) * | 1998-12-10 | 2000-06-21 | Hughes Electronics Corporation | Method and system for incorporating two-way ranging navigation as a calibration reference for GPS |
Also Published As
Publication number | Publication date |
---|---|
WO2007086899A2 (en) | 2007-08-02 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
WO2007086899A3 (en) | Transponder landing system augmentation of the global positioning system | |
US11327181B2 (en) | Method and apparatus for accurate reporting of integrity of GNSS-based positioning system | |
CN103134491B (en) | GEO orbit transfer vehicle SINS/CNS/GNSS integrated navigation system | |
EP1537434B1 (en) | Position computation in a positioning system using synchronization time bias | |
WO2018063245A8 (en) | Autonomous vehicle: vehicle localization | |
WO2003025617A3 (en) | Annunciation of the distance to a target position in a gps landing system | |
CN101535833B (en) | Mobile unit positioning device | |
WO2007067192A3 (en) | Precision approach guidance system and associated method | |
EP1980869A3 (en) | Navigation guidance for aircraft approach and landing | |
WO2005062070A2 (en) | Method and system for a data interface for aiding a satellite positioning system receiver | |
CN106255065A (en) | Smart mobile phone and the seamless alignment system of mobile terminal indoor and outdoor and method thereof | |
ATE222001T1 (en) | VEHICLE LOCATION SYSTEM USING A GPS-TYPE SATELLITE NAVIGATION SYSTEM | |
CN109991632B (en) | Positioning system and method | |
CN103149571B (en) | GNSS (Global Navigation Satellite System)-based signal aided time frequency difference comprehensive correction method | |
WO2008097346A3 (en) | Method for fusing multiple gps measurement types into a weighted least squares solution | |
CN104459745A (en) | Quick resolving method for multi-constellation long-base-line network RTK partial ambiguity | |
CN102778686A (en) | Synergic vehicle positioning method based on mobile global positioning system (GPS)/inertial navigation system (INS) node | |
CN110907976A (en) | High-speed railway combined navigation system based on Beidou satellite | |
CN106093992A (en) | A kind of sub-meter grade combined positioning and navigating system based on CORS and air navigation aid | |
WO2002091014A3 (en) | A gps based terrain referenced navigation system | |
Du et al. | Integration of PPP GPS and low cost IMU | |
US11187814B2 (en) | Method and device for increasing the accuracy of localization | |
WO2009011611A8 (en) | Airplane landing method using a satellite navigation system and a landing system based thereon | |
WO2012062723A3 (en) | Method for determining the altitude profile of a section of track for a rail vehicle | |
Liu et al. | Robust train localisation method based on advanced map matching measurement-augmented tightly-coupled GNSS/INS with error-state UKF |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
NENP | Non-entry into the national phase |
Ref country code: DE |
|
NENP | Non-entry into the national phase |
Ref country code: RU |
|
121 | Ep: the epo has been informed by wipo that ep was designated in this application |
Ref document number: 06849751 Country of ref document: EP Kind code of ref document: A2 |
|
122 | Ep: pct application non-entry in european phase |
Ref document number: 06849751 Country of ref document: EP Kind code of ref document: A2 |