ATE528705T1 - Implementierung kontinuierlicher landeanflüge für maximale vorhersagbarkeit bei flugzeugen - Google Patents
Implementierung kontinuierlicher landeanflüge für maximale vorhersagbarkeit bei flugzeugenInfo
- Publication number
- ATE528705T1 ATE528705T1 AT09380031T AT09380031T ATE528705T1 AT E528705 T1 ATE528705 T1 AT E528705T1 AT 09380031 T AT09380031 T AT 09380031T AT 09380031 T AT09380031 T AT 09380031T AT E528705 T1 ATE528705 T1 AT E528705T1
- Authority
- AT
- Austria
- Prior art keywords
- predictability
- implementation
- continuous descent
- approaches
- arrival time
- Prior art date
Links
- 238000013459 approach Methods 0.000 abstract 3
- 230000003466 anti-cipated effect Effects 0.000 abstract 1
- 230000001447 compensatory effect Effects 0.000 abstract 1
- 238000005381 potential energy Methods 0.000 abstract 1
Classifications
-
- 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
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/80—Energy efficient operational measures, e.g. ground operations or mission management
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Automation & Control Theory (AREA)
- Traffic Control Systems (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| EP09380031A EP2224305B1 (en) | 2009-02-25 | 2009-02-25 | Implementing continuous descent approaches for maximum predictability in aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| ATE528705T1 true ATE528705T1 (de) | 2011-10-15 |
Family
ID=41393638
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| AT09380031T ATE528705T1 (de) | 2009-02-25 | 2009-02-25 | Implementierung kontinuierlicher landeanflüge für maximale vorhersagbarkeit bei flugzeugen |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US8442707B2 (enExample) |
| EP (1) | EP2224305B1 (enExample) |
| JP (1) | JP5473672B2 (enExample) |
| AT (1) | ATE528705T1 (enExample) |
| ES (1) | ES2371321T3 (enExample) |
Families Citing this family (21)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| ES2324561T5 (es) * | 2007-02-23 | 2012-10-19 | The Boeing Company | Implementación de aproximaciones de descenso continuo para máxima previsibilidad en aeronaves |
| EP2282247B1 (en) * | 2009-05-05 | 2019-07-10 | The Boeing Company | Four-dimensional guidance of an aircraft |
| FR2949897B1 (fr) * | 2009-09-04 | 2012-08-03 | Thales Sa | Procede d'assistance au pilotage d'un aeronef et dispositif correspondant. |
| ES2485294T3 (es) * | 2010-08-24 | 2014-08-13 | The Boeing Company | Guiado en cuatro dimensiones de una aeronave |
| US9442490B2 (en) * | 2011-04-29 | 2016-09-13 | Airbus Engineering Centre India | System and method for aircraft performance predictions for descent and approach phases |
| US8467918B2 (en) * | 2011-07-05 | 2013-06-18 | Universal Avionics Systems Corporation | Heuristic method for computing performance of an aircraft |
| FR2978587B1 (fr) * | 2011-07-29 | 2016-03-11 | Airbus Operations Sas | Procede et dispositif de gestion optimisee de l'energie d'un aeronef |
| FR2978588B1 (fr) * | 2011-07-29 | 2016-03-11 | Airbus Operations Sas | Procede et dispositif de gestion optimisee de l'utilisation des becs et des volets, ainsi que du train d'atterrissage d'un aeronef |
| US20130096845A1 (en) | 2011-10-14 | 2013-04-18 | Ze'ev Russak | Cumulative differential chemical assay identification |
| US9026275B1 (en) * | 2013-07-24 | 2015-05-05 | Shih-Yih Young | In-flight generation of RTA-compliant optimal profile descent paths |
| US9424756B2 (en) * | 2013-09-14 | 2016-08-23 | The Boeing Company | Visual flight rules approach to airports |
| US9262930B2 (en) | 2014-03-18 | 2016-02-16 | The Boeing Company | Arrival Traffic scheduling system incorporating equipage-dependent in-trial spacing |
| US10475346B1 (en) * | 2014-10-08 | 2019-11-12 | United States Of America As Represented By The Administrator Of Nasa | Miles-in-trail with passback restrictions for use in air traffic management |
| US10347142B2 (en) | 2014-11-05 | 2019-07-09 | Honeywell International Inc. | Air traffic system using procedural trajectory prediction |
| US9418561B2 (en) | 2014-12-02 | 2016-08-16 | Honeywell International Inc. | System and method for displaying predictive conformal configuration cues for executing a landing |
| ES2707449T3 (es) | 2015-06-26 | 2019-04-03 | Boeing Co | Método y sistema para controlar el vuelo de una aeronave sometida a al menos dos tiempos requeridos de restricciones de llegada |
| EP3109724B1 (en) | 2015-06-26 | 2022-02-09 | The Boeing Company | Method and system of controlling a flight of an aircraft subjected to a required time of arrival constraint |
| US9898934B2 (en) | 2016-07-25 | 2018-02-20 | Honeywell International Inc. | Prediction of vehicle maneuvers |
| US10228692B2 (en) | 2017-03-27 | 2019-03-12 | Gulfstream Aerospace Corporation | Aircraft flight envelope protection and recovery autopilot |
| US11269957B2 (en) | 2019-03-28 | 2022-03-08 | Tetra Tech, Inc. | Method for creating a data input file for increasing the efficiency of the aviation environmental design tool (AEDT) |
| CN112800897B (zh) * | 2021-01-18 | 2023-12-26 | 深圳市瑞达飞行科技有限公司 | 连续下降运行的识别方法、识别装置和电子设备 |
Family Cites Families (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3789661A (en) * | 1970-06-25 | 1974-02-05 | F Melsheimer | Aircraft glide angle and rate of change of total energy indication means |
| US4709336A (en) * | 1985-01-09 | 1987-11-24 | Sperry Corporation | Descent flight path control for aircraft |
| US4956780A (en) * | 1988-12-08 | 1990-09-11 | The Boeing Company | Flight path angle command flight control system for landing flare |
| JP2923509B2 (ja) * | 1994-08-24 | 1999-07-26 | 科学技術庁長官官房会計課長 | 航空機の着陸支援方法及び装置 |
| DE19604931A1 (de) * | 1996-02-10 | 1997-08-14 | Nfs Navigations Und Flugfuehru | Verfahren zur Korrektur des Flugablaufs eines Fluggerätes |
| US6038497A (en) * | 1996-11-18 | 2000-03-14 | Trimble Navigation Limited | Aircraft turn guidance system |
| US5745054A (en) * | 1996-11-18 | 1998-04-28 | Honeywell Inc. | Method and apparatus for conformal runway alignment on a head up display |
| US6389333B1 (en) * | 1997-07-09 | 2002-05-14 | Massachusetts Institute Of Technology | Integrated flight information and control system |
| US6282466B1 (en) * | 1998-11-03 | 2001-08-28 | The Boeing Company | Method of automated thrust-based roll guidance limiting |
| US8027758B2 (en) * | 2005-01-19 | 2011-09-27 | Airbus Operations (S.A.S.) | Navigation system for an aircraft and associated command process |
| FR2885439B1 (fr) * | 2005-05-09 | 2010-11-19 | Airbus France | Procede et dispositif d'aide au pilotage d'un avion lors d'une phase d'approche en vue d'un atterrissage |
| US7706932B2 (en) * | 2006-11-30 | 2010-04-27 | Instituto Nacional de Tecnica Aeroespacial “Estaban Terradas” | Method for controlling control parameters in an air vehicle and system of controlling an air vehicle |
| ES2324561T5 (es) * | 2007-02-23 | 2012-10-19 | The Boeing Company | Implementación de aproximaciones de descenso continuo para máxima previsibilidad en aeronaves |
| US20090112535A1 (en) * | 2007-10-26 | 2009-04-30 | Sensis Corporation | Method of integrating point mass equations to include vertical and horizontal profiles |
-
2009
- 2009-02-25 ES ES09380031T patent/ES2371321T3/es active Active
- 2009-02-25 AT AT09380031T patent/ATE528705T1/de not_active IP Right Cessation
- 2009-02-25 EP EP09380031A patent/EP2224305B1/en active Active
-
2010
- 2010-02-11 US US12/704,274 patent/US8442707B2/en active Active
- 2010-02-25 JP JP2010039652A patent/JP5473672B2/ja active Active
Also Published As
| Publication number | Publication date |
|---|---|
| JP2010195392A (ja) | 2010-09-09 |
| EP2224305B1 (en) | 2011-10-12 |
| US20100217461A1 (en) | 2010-08-26 |
| US8442707B2 (en) | 2013-05-14 |
| ES2371321T3 (es) | 2011-12-29 |
| EP2224305A1 (en) | 2010-09-01 |
| JP5473672B2 (ja) | 2014-04-16 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| RER | Ceased as to paragraph 5 lit. 3 law introducing patent treaties |