ATE526592T1 - Verfahren und vorrichtung zur landehilfe eines flugzeuges auf eine landebahn - Google Patents
Verfahren und vorrichtung zur landehilfe eines flugzeuges auf eine landebahnInfo
- Publication number
- ATE526592T1 ATE526592T1 AT05290677T AT05290677T ATE526592T1 AT E526592 T1 ATE526592 T1 AT E526592T1 AT 05290677 T AT05290677 T AT 05290677T AT 05290677 T AT05290677 T AT 05290677T AT E526592 T1 ATE526592 T1 AT E526592T1
- Authority
- AT
- Austria
- Prior art keywords
- aircraft
- distance
- landing
- height
- threshold
- 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
- G01S19/13—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
- G01S1/00—Beacons or beacon systems transmitting signals having a characteristic or characteristics capable of being detected by non-directional receivers and defining directions, positions, or position lines fixed relatively to the beacon transmitters; Receivers co-operating therewith
- G01S1/02—Beacons or beacon systems transmitting signals having a characteristic or characteristics capable of being detected by non-directional receivers and defining directions, positions, or position lines fixed relatively to the beacon transmitters; Receivers co-operating therewith using radio waves
- G01S1/08—Systems for determining direction or position line
- G01S1/14—Systems for determining direction or position line using amplitude comparison of signals transmitted simultaneously from antennas or antenna systems having differently oriented overlapping directivity-characteristics
- G01S1/18—Elevational guidance systems, e.g. system for defining aircraft glide path
-
- 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
- G01S1/00—Beacons or beacon systems transmitting signals having a characteristic or characteristics capable of being detected by non-directional receivers and defining directions, positions, or position lines fixed relatively to the beacon transmitters; Receivers co-operating therewith
- G01S1/02—Beacons or beacon systems transmitting signals having a characteristic or characteristics capable of being detected by non-directional receivers and defining directions, positions, or position lines fixed relatively to the beacon transmitters; Receivers co-operating therewith using radio waves
- G01S1/08—Systems for determining direction or position line
- G01S1/44—Rotating or oscillating beam beacons defining directions in the plane of rotation or oscillation
- G01S1/54—Narrow-beam systems producing at a receiver a pulse-type envelope signal of the carrier wave of the beam, the timing of which is dependent upon the angle between the direction of the receiver from the beacon and a reference direction from the beacon; Overlapping broad beam systems defining a narrow zone and producing at a receiver a pulse-type envelope signal of the carrier wave of the beam, the timing of which is dependent upon the angle between the direction of the receiver from the beacon and a reference direction from the beacon
- G01S1/56—Timing the pulse-type envelope signals derived by reception of the beam
-
- 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
- G01S19/396—Determining accuracy or reliability of position or pseudorange measurements
Landscapes
- Engineering & Computer Science (AREA)
- Remote Sensing (AREA)
- Radar, Positioning & Navigation (AREA)
- Computer Networks & Wireless Communication (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Aviation & Aerospace Engineering (AREA)
- Traffic Control Systems (AREA)
- Position Fixing By Use Of Radio Waves (AREA)
- Tents Or Canopies (AREA)
- Variable-Direction Aerials And Aerial Arrays (AREA)
- Road Paving Structures (AREA)
- Radar Systems Or Details Thereof (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR0404268A FR2869419B1 (fr) | 2004-04-22 | 2004-04-22 | Procede et dispositif d'aide a l'atterrissage d'un aeronef sur une piste d'atterrissage |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| ATE526592T1 true ATE526592T1 (de) | 2011-10-15 |
Family
ID=34942041
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| AT05290677T ATE526592T1 (de) | 2004-04-22 | 2005-03-29 | Verfahren und vorrichtung zur landehilfe eines flugzeuges auf eine landebahn |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US7286077B2 (de) |
| EP (1) | EP1589351B1 (de) |
| AT (1) | ATE526592T1 (de) |
| CA (1) | CA2502618C (de) |
| FR (1) | FR2869419B1 (de) |
Families Citing this family (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2005059656A (ja) * | 2003-08-08 | 2005-03-10 | Fuji Heavy Ind Ltd | 飛行体の着陸制御装置および飛行体の着陸制御方法 |
| 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. |
| US20080133074A1 (en) * | 2006-12-01 | 2008-06-05 | Zyss Michael J | Autonomous rollout control of air vehicle |
| FR2917221B1 (fr) | 2007-06-11 | 2014-01-17 | Airbus France | Systeme de guidage et de pilotage d'un aeronef en cas d'incapacite des pilotes a controler l'aeronef |
| FR2925712B1 (fr) * | 2007-12-21 | 2010-01-01 | Thales Sa | Procede pour l'aide a l'atterrissage d'aeronef utilisant un gps et un mls dans le cadre d'une approche axiale calculee. |
| DE102008033235A1 (de) * | 2008-07-15 | 2010-03-11 | Astrium Gmbh | Verfahren zum automatischen Ermitteln einer Landebahn |
| US8494693B2 (en) * | 2009-08-05 | 2013-07-23 | The Boeing Company | Vertical required navigation performance containment with radio altitude |
| US9134403B1 (en) * | 2013-02-20 | 2015-09-15 | The United States Of America As Represented By The Secretary Of The Navy | System and method for relative localization |
| FR3039691B1 (fr) * | 2015-07-31 | 2017-07-21 | Airbus Operations Sas | Procede et systeme d'aide au guidage d'un aeronef le long d'un axe d'approche d'une piste d'atterrissage |
| FR3061794B1 (fr) * | 2017-01-06 | 2019-05-24 | Thales | Dispositif electronique de surveillance d'au moins un signal de radionavigation en phase d'approche d'une piste d'atterrissage, procede de surveillance et programme d'ordinateur associes |
| US20250348087A1 (en) * | 2024-05-13 | 2025-11-13 | University Of Washington | Generation of approach and landing trajectories with operational constraints for aircraft with multiple degrees of freedom |
Family Cites Families (16)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3662392A (en) * | 1970-12-08 | 1972-05-09 | Boeing Co | Glide slope antenna system |
| US4667196A (en) * | 1984-06-13 | 1987-05-19 | Kaul Charles E | Active visual display system for remote three-axis flight path guidance of landing aircraft |
| FR2611399B1 (fr) * | 1987-02-27 | 1994-06-17 | Lmt Radio Professionelle | Systeme d'aide a l'atterrissage mettant en oeuvre des satellites de navigation |
| US5361212A (en) * | 1992-11-02 | 1994-11-01 | Honeywell Inc. | Differential GPS landing assistance system |
| FR2718875B1 (fr) * | 1994-04-15 | 1996-05-15 | Sextant Avionique | Dispositif d'aide à l'atterrissage. |
| FR2725808B1 (fr) * | 1994-10-18 | 1997-01-03 | Sextant Avionique | Dispositif optoelectronique d'aide au pilotage d'un aeronef |
| US5748136A (en) * | 1995-09-22 | 1998-05-05 | Rockwell International Corporation | Electronic landmark enhancement to GPS based navigation systems |
| JP2743905B2 (ja) * | 1996-02-28 | 1998-04-28 | 日本電気株式会社 | 監視空間通過検出装置 |
| US5820080A (en) * | 1996-03-14 | 1998-10-13 | Trimble Navigation Limited | Precision equivalent landing system using gps and an altimeter |
| US6178363B1 (en) * | 1998-12-22 | 2001-01-23 | The Boeing Company | Inertially augmented GPS landing system |
| US6239745B1 (en) * | 1999-07-30 | 2001-05-29 | Rockwell Collins, Inc. | Satellite landing system having instrument landing system look alike guidance |
| US6157876A (en) * | 1999-10-12 | 2000-12-05 | Honeywell International Inc. | Method and apparatus for navigating an aircraft from an image of the runway |
| WO2003077224A1 (en) * | 2001-10-11 | 2003-09-18 | Sandel Avionics, Llc | Method and apparatus for reducing false taws warnings |
| US6711479B1 (en) | 2001-08-30 | 2004-03-23 | Honeywell International, Inc. | Avionics system for determining terminal flightpath |
| US6862519B2 (en) * | 2001-12-04 | 2005-03-01 | Smiths Aerospace, Inc. | Airport map system with compact feature data storage |
| FR2852684B1 (fr) * | 2003-03-19 | 2005-05-20 | Airbus France | Procede et dispositif pour determiner un axe d'approche finale d'un aeronef pour une approche de non precision en vue d'un atterrissage de l'aeronef. |
-
2004
- 2004-04-22 FR FR0404268A patent/FR2869419B1/fr not_active Expired - Fee Related
-
2005
- 2005-03-29 EP EP05290677A patent/EP1589351B1/de not_active Expired - Lifetime
- 2005-03-29 AT AT05290677T patent/ATE526592T1/de not_active IP Right Cessation
- 2005-04-06 CA CA2502618A patent/CA2502618C/fr not_active Expired - Fee Related
- 2005-04-18 US US11/108,116 patent/US7286077B2/en not_active Expired - Lifetime
Also Published As
| Publication number | Publication date |
|---|---|
| CA2502618C (fr) | 2012-09-25 |
| CA2502618A1 (fr) | 2005-10-22 |
| US7286077B2 (en) | 2007-10-23 |
| US20050237235A1 (en) | 2005-10-27 |
| EP1589351B1 (de) | 2011-09-28 |
| EP1589351A1 (de) | 2005-10-26 |
| FR2869419A1 (fr) | 2005-10-28 |
| FR2869419B1 (fr) | 2006-06-30 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| RER | Ceased as to paragraph 5 lit. 3 law introducing patent treaties |