FR2916074B1 - Procede et dispositif de detection de bruit sur un signal de guidage de type loc recu par un aeronef - Google Patents
Procede et dispositif de detection de bruit sur un signal de guidage de type loc recu par un aeronefInfo
- Publication number
- FR2916074B1 FR2916074B1 FR0754946A FR0754946A FR2916074B1 FR 2916074 B1 FR2916074 B1 FR 2916074B1 FR 0754946 A FR0754946 A FR 0754946A FR 0754946 A FR0754946 A FR 0754946A FR 2916074 B1 FR2916074 B1 FR 2916074B1
- Authority
- FR
- France
- Prior art keywords
- aircraft
- signal received
- detecting noise
- type guiding
- guiding signal
- 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.)
- Expired - Fee Related
Links
Classifications
-
- G—PHYSICS
- G08—SIGNALLING
- G08G—TRAFFIC CONTROL SYSTEMS
- G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
- G08G5/02—Automatic approach or landing aids, i.e. systems in which flight data of incoming planes are processed to provide landing data
- G08G5/025—Navigation or guidance aids
-
- 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
- G01S1/022—Means for monitoring or calibrating
- G01S1/026—Means for monitoring or calibrating of associated receivers
-
- 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
- G01S1/16—Azimuthal guidance systems, e.g. system for defining aircraft approach path, localiser system
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
- G05D1/02—Control of position or course in two dimensions
- G05D1/0202—Control of position or course in two dimensions specially adapted to aircraft
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0754946A FR2916074B1 (fr) | 2007-05-09 | 2007-05-09 | Procede et dispositif de detection de bruit sur un signal de guidage de type loc recu par un aeronef |
US12/109,903 US8239077B2 (en) | 2007-05-09 | 2008-04-25 | Method and device for detecting noise on a guide signal of LOC type received by an aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0754946A FR2916074B1 (fr) | 2007-05-09 | 2007-05-09 | Procede et dispositif de detection de bruit sur un signal de guidage de type loc recu par un aeronef |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2916074A1 FR2916074A1 (fr) | 2008-11-14 |
FR2916074B1 true FR2916074B1 (fr) | 2009-07-03 |
Family
ID=38783526
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR0754946A Expired - Fee Related FR2916074B1 (fr) | 2007-05-09 | 2007-05-09 | Procede et dispositif de detection de bruit sur un signal de guidage de type loc recu par un aeronef |
Country Status (2)
Country | Link |
---|---|
US (1) | US8239077B2 (fr) |
FR (1) | FR2916074B1 (fr) |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2929246B1 (fr) * | 2008-03-26 | 2010-03-05 | Airbus France | Procede et dispositif pour la detection d'absences de pilotage manuel et automatique d'un aeronef |
US20100082180A1 (en) * | 2008-10-01 | 2010-04-01 | Honeywell International Inc. | Errant vehicle countermeasures |
US8983677B2 (en) | 2008-10-01 | 2015-03-17 | Honeywell International Inc. | Acoustic fingerprinting of mechanical devices |
US8958932B2 (en) * | 2013-02-11 | 2015-02-17 | The Boeing Company | Methods and apparatus to mitigate instrument landing system overflight interference |
FR3044811B1 (fr) | 2015-12-08 | 2018-01-12 | Airbus Operations | Procede et dispositif d'estimation d'une vitesse laterale et d'une position laterale d'un aeronef, lors d'une phase de roulage de l'aeronef. |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3788579A (en) * | 1972-03-10 | 1974-01-29 | Bendix Corp | Aircraft control system using inertially sensed data |
US3918662A (en) * | 1974-01-21 | 1975-11-11 | Boeing Co | Localizer lateral guidance control system |
US4482961A (en) * | 1981-09-18 | 1984-11-13 | The Boeing Company | Automatic control system for directional control of an aircraft during landing rollout |
US5014053A (en) * | 1990-01-18 | 1991-05-07 | The Boeing Company | Method and apparatus for determining actual lateral deviation from runway centerline |
US6711479B1 (en) * | 2001-08-30 | 2004-03-23 | Honeywell International, Inc. | Avionics system for determining terminal flightpath |
US7364121B2 (en) * | 2005-03-14 | 2008-04-29 | The Boeing Company | Methods and systems for automatically controlling aircraft takeoff rolls |
-
2007
- 2007-05-09 FR FR0754946A patent/FR2916074B1/fr not_active Expired - Fee Related
-
2008
- 2008-04-25 US US12/109,903 patent/US8239077B2/en active Active
Also Published As
Publication number | Publication date |
---|---|
US20090005920A1 (en) | 2009-01-01 |
FR2916074A1 (fr) | 2008-11-14 |
US8239077B2 (en) | 2012-08-07 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
CA | Change of address |
Effective date: 20110916 |
|
CD | Change of name or company name |
Owner name: AIRBUS HOLDING, FR Effective date: 20110916 |
|
CJ | Change in legal form |
Effective date: 20110916 |
|
TP | Transmission of property |
Owner name: AIRBUS HOLDING, FR Effective date: 20110913 |
|
PLFP | Fee payment |
Year of fee payment: 10 |
|
PLFP | Fee payment |
Year of fee payment: 11 |
|
PLFP | Fee payment |
Year of fee payment: 12 |
|
PLFP | Fee payment |
Year of fee payment: 13 |
|
ST | Notification of lapse |
Effective date: 20210105 |