ATE348317T1 - Flugzeuglandewinkelüberwachungseinrichtung - Google Patents
FlugzeuglandewinkelüberwachungseinrichtungInfo
- Publication number
- ATE348317T1 ATE348317T1 AT01963758T AT01963758T ATE348317T1 AT E348317 T1 ATE348317 T1 AT E348317T1 AT 01963758 T AT01963758 T AT 01963758T AT 01963758 T AT01963758 T AT 01963758T AT E348317 T1 ATE348317 T1 AT E348317T1
- Authority
- AT
- Austria
- Prior art keywords
- aircraft
- runway
- component configured
- approach angle
- approach
- Prior art date
Links
- 238000012806 monitoring device Methods 0.000 title 1
- 238000004590 computer program Methods 0.000 abstract 1
- 238000000034 method Methods 0.000 abstract 1
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
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C5/00—Measuring height; Measuring distances transverse to line of sight; Levelling between separated points; Surveyors' levels
- G01C5/005—Measuring height; Measuring distances transverse to line of sight; Levelling between separated points; Surveyors' levels altimeters for aircraft
-
- 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
-
- 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
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- G05D1/04—Control of altitude or depth
- G05D1/06—Rate of change of altitude or depth
- G05D1/0607—Rate of change of altitude or depth specially adapted for aircraft
- G05D1/0653—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing
- G05D1/0676—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing specially adapted for landing
Landscapes
- Engineering & Computer Science (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Radar, Positioning & Navigation (AREA)
- Aviation & Aerospace Engineering (AREA)
- Computer Networks & Wireless Communication (AREA)
- Automation & Control Theory (AREA)
- Traffic Control Systems (AREA)
- A Measuring Device Byusing Mechanical Method (AREA)
- Variable-Direction Aerials And Aerial Arrays (AREA)
- Maintenance And Inspection Apparatuses For Elevators (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US22640000P | 2000-08-18 | 2000-08-18 |
Publications (1)
Publication Number | Publication Date |
---|---|
ATE348317T1 true ATE348317T1 (de) | 2007-01-15 |
Family
ID=22848761
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
AT01963758T ATE348317T1 (de) | 2000-08-18 | 2001-07-27 | Flugzeuglandewinkelüberwachungseinrichtung |
Country Status (5)
Country | Link |
---|---|
US (1) | US6600977B2 (de) |
EP (1) | EP1309837B1 (de) |
AT (1) | ATE348317T1 (de) |
DE (1) | DE60125187T2 (de) |
WO (1) | WO2002016870A2 (de) |
Families Citing this family (30)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE60132070T2 (de) * | 2000-02-03 | 2008-12-18 | Honeywell International Inc. | Verfahren, gerät und rechnerprogramm zur warnung eines nichtstabilisierten anflugs |
US8145367B2 (en) | 2001-03-06 | 2012-03-27 | Honeywell International Inc. | Closed airport surface alerting system |
US7587278B2 (en) * | 2002-05-15 | 2009-09-08 | Honeywell International Inc. | Ground operations and advanced runway awareness and advisory system |
US7079951B2 (en) * | 2002-05-15 | 2006-07-18 | Honeywell International Inc. | Ground operations and imminent landing runway selection |
US20040167685A1 (en) * | 2003-02-24 | 2004-08-26 | Ryan Dean E. | Runway overrun monitor and method for monitoring runway overruns |
US6718236B1 (en) * | 2003-04-29 | 2004-04-06 | The Mitre Corporation | Method for conducting a moving vehicle along a trajectory of a coordinated maneuver based on state information broadcast by other vehicles participating in the coordinated maneuver |
US7783393B2 (en) * | 2004-06-30 | 2010-08-24 | The Boeing Company | Enhanced vertical situation display |
FR2897593B1 (fr) * | 2006-02-17 | 2012-09-14 | Airbus France | Procede et systeme pour predire la possibilite d'arret complet d'un aeronef sur une piste d'atterrissage. |
US7546183B1 (en) * | 2006-03-10 | 2009-06-09 | Frank Marcum | In-flight verification of instrument landing system signals |
FR2911988B1 (fr) * | 2007-01-26 | 2016-03-25 | Airbus France | Procede et dispositif pour determiner une hauteur maximale de stabilisation lors de la phase finale de vol d'un avion |
US7852236B2 (en) * | 2008-07-31 | 2010-12-14 | Honeywell International Inc. | Aircraft synthetic vision system for approach and landing |
US20100036550A1 (en) * | 2008-08-05 | 2010-02-11 | Honeywell International Inc. | Systems and methods for improving pilot situational awareness during landing |
US8116923B2 (en) * | 2009-11-19 | 2012-02-14 | Honeywell International | Stabilized approach monitor |
FR2968818B1 (fr) * | 2010-12-08 | 2014-07-11 | Airbus Operations Sas | Procede et dispositif d'aide a l'approche d'un aeronef lors d'une approche en vue d'un atterrissage. |
US8630756B2 (en) * | 2011-04-12 | 2014-01-14 | The Boeing Company | Airplane position assurance monitor |
US8774985B2 (en) | 2011-07-22 | 2014-07-08 | The Boeing Company | Systems and methods for generating a command trajectory |
US8798820B2 (en) * | 2011-09-08 | 2014-08-05 | The Boeing Company | Consistent localizer captures |
US9527601B2 (en) | 2013-02-05 | 2016-12-27 | Honeywell International Inc. | Method and apparatus for generating a virtual inner marker for an aircraft landing approach |
US9098999B2 (en) * | 2013-09-13 | 2015-08-04 | The Boeing Company | Systems and methods for assuring the accuracy of a synthetic runway presentation |
FR3013882B1 (fr) * | 2013-11-28 | 2016-01-08 | Thales Sa | Dispositif de surveillance de la stabilisation de la phase d'approche d'un aeronef vers une piste d'atterrissage, procede et produit programme d'ordinateur associes |
US9522742B2 (en) | 2014-03-18 | 2016-12-20 | The Boeing Company | Short landing warning |
US9269272B2 (en) * | 2014-03-27 | 2016-02-23 | Honeywell International Inc. | Independent instrument landing system monitor |
JP6438209B2 (ja) * | 2014-04-07 | 2018-12-12 | 株式会社荏原製作所 | 検査装置において撮像装置用のタイミング信号を生成するための制御装置、撮像装置にタイミング信号を送出する方法 |
RU2567240C1 (ru) * | 2014-05-30 | 2015-11-10 | Федеральное государственное казенное военное образовательное учреждение высшего профессионального образования "Военная академия Ракетных войск стратегического назначения имени Петра Великого" Министерства обороны Российской Федерации | Способ измерения угла крена летательного аппарата |
US9646506B2 (en) | 2015-09-30 | 2017-05-09 | Honeywell International Inc. | Methods and apparatus for managing a premature descent envelope during descent of an aircraft |
US9916765B2 (en) | 2015-11-04 | 2018-03-13 | Honeywell International Inc. | Aircraft systems and methods for providing landing approach alerts |
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 |
US10228692B2 (en) | 2017-03-27 | 2019-03-12 | Gulfstream Aerospace Corporation | Aircraft flight envelope protection and recovery autopilot |
FR3072490B1 (fr) * | 2017-10-17 | 2019-11-08 | Airbus Operations (S.A.S.) | Systeme et procede d'aide a l'atterrissage d'un aeronef |
US11107361B1 (en) * | 2020-06-30 | 2021-08-31 | Honeywell International Inc. | Systems and methods for alerting for an instrument landing system (ILS) |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3678256A (en) * | 1970-10-05 | 1972-07-18 | Mc Donnell Douglas Corp | Performance and failure assessment monitor |
US3750176A (en) * | 1971-10-05 | 1973-07-31 | Bendix Corp | Integrity monitor for ils receiver with automatic change of monitor threshold sensitivity |
US3947809A (en) * | 1975-01-13 | 1976-03-30 | Sundstrand Data Control, Inc. | Below glide slope advisory warning system for aircraft |
US5631656A (en) * | 1995-03-01 | 1997-05-20 | Honeywell Inc. | Fail safe system with common mode avoidance |
US5820080A (en) * | 1996-03-14 | 1998-10-13 | Trimble Navigation Limited | Precision equivalent landing system using gps and an altimeter |
-
2001
- 2001-07-27 EP EP01963758A patent/EP1309837B1/de not_active Expired - Lifetime
- 2001-07-27 WO PCT/US2001/023975 patent/WO2002016870A2/en active IP Right Grant
- 2001-07-27 AT AT01963758T patent/ATE348317T1/de not_active IP Right Cessation
- 2001-07-27 DE DE60125187T patent/DE60125187T2/de not_active Expired - Fee Related
- 2001-07-27 US US09/916,633 patent/US6600977B2/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
EP1309837A2 (de) | 2003-05-14 |
US6600977B2 (en) | 2003-07-29 |
DE60125187D1 (de) | 2007-01-25 |
US20020040263A1 (en) | 2002-04-04 |
WO2002016870A3 (en) | 2002-05-10 |
WO2002016870A2 (en) | 2002-02-28 |
EP1309837B1 (de) | 2006-12-13 |
DE60125187T2 (de) | 2007-11-15 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
RER | Ceased as to paragraph 5 lit. 3 law introducing patent treaties |