FR2949897B1 - Procede d'assistance au pilotage d'un aeronef et dispositif correspondant. - Google Patents
Procede d'assistance au pilotage d'un aeronef et dispositif correspondant.Info
- Publication number
- FR2949897B1 FR2949897B1 FR0904211A FR0904211A FR2949897B1 FR 2949897 B1 FR2949897 B1 FR 2949897B1 FR 0904211 A FR0904211 A FR 0904211A FR 0904211 A FR0904211 A FR 0904211A FR 2949897 B1 FR2949897 B1 FR 2949897B1
- Authority
- FR
- France
- Prior art keywords
- aircraft
- corresponding device
- assistance method
- assisting
- assisting assistance
- 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.)
- Active
Links
Classifications
-
- G—PHYSICS
- G08—SIGNALLING
- G08G—TRAFFIC CONTROL SYSTEMS
- G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
- G08G5/04—Anti-collision systems
- G08G5/045—Navigation or guidance aids, e.g. determination of anti-collision manoeuvers
-
- G—PHYSICS
- G08—SIGNALLING
- G08G—TRAFFIC CONTROL SYSTEMS
- G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
- G08G5/0047—Navigation or guidance aids for a single aircraft
- G08G5/0056—Navigation or guidance aids for a single aircraft in an emergency situation, e.g. hijacking
-
- G—PHYSICS
- G08—SIGNALLING
- G08G—TRAFFIC CONTROL SYSTEMS
- G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
- G08G5/06—Traffic control systems for aircraft, e.g. air-traffic control [ATC] for control when on the ground
- G08G5/065—Navigation or guidance aids, e.g. for taxiing or rolling
Landscapes
- Engineering & Computer Science (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Aviation & Aerospace Engineering (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Business, Economics & Management (AREA)
- Emergency Management (AREA)
- Traffic Control Systems (AREA)
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0904211A FR2949897B1 (fr) | 2009-09-04 | 2009-09-04 | Procede d'assistance au pilotage d'un aeronef et dispositif correspondant. |
US12/876,952 US8849478B2 (en) | 2009-09-04 | 2010-09-07 | Aircraft piloting assistance method and corresponding device |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0904211A FR2949897B1 (fr) | 2009-09-04 | 2009-09-04 | Procede d'assistance au pilotage d'un aeronef et dispositif correspondant. |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2949897A1 FR2949897A1 (fr) | 2011-03-11 |
FR2949897B1 true FR2949897B1 (fr) | 2012-08-03 |
Family
ID=42115830
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR0904211A Active FR2949897B1 (fr) | 2009-09-04 | 2009-09-04 | Procede d'assistance au pilotage d'un aeronef et dispositif correspondant. |
Country Status (2)
Country | Link |
---|---|
US (1) | US8849478B2 (fr) |
FR (1) | FR2949897B1 (fr) |
Families Citing this family (20)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2920580B1 (fr) * | 2007-08-31 | 2010-09-03 | Thales Sa | Procede de simplification de l'affichage d'elements stationnaires d'une base de donnees embarquee |
US9934692B2 (en) * | 2012-02-22 | 2018-04-03 | Honeywell International Inc. | Display system and method for generating a display |
FR3006785B1 (fr) * | 2013-06-10 | 2015-07-03 | Snecma | Procedes de creation d'une base de donnees et d'elaboration d'une carte d'etats de fonctionnement de moteurs d'aeronefs, et un procede de surveillance du fonctionnement d'un moteur d'aeronef associe |
US9026275B1 (en) * | 2013-07-24 | 2015-05-05 | Shih-Yih Young | In-flight generation of RTA-compliant optimal profile descent paths |
FR3043487B1 (fr) * | 2015-11-06 | 2018-05-18 | Thales | Gestion de trajectoire d'un aeronef en cas de panne moteur |
US10096253B2 (en) | 2015-11-30 | 2018-10-09 | Honeywell International Inc. | Methods and systems for presenting diversion destinations |
US10134292B2 (en) * | 2015-12-07 | 2018-11-20 | Airbus Group India Private Limited | Navigating and guiding an aircraft to a reachable airport during complete engine failure |
US10152195B2 (en) | 2015-12-14 | 2018-12-11 | Honeywell International Inc. | Aircraft display system pertaining to energy management |
US10304344B2 (en) | 2016-02-09 | 2019-05-28 | Honeywell International Inc. | Methods and systems for safe landing at a diversion airport |
US9640079B1 (en) | 2016-02-09 | 2017-05-02 | Honeywell International Inc. | Methods and systems facilitating holding for an unavailable destination |
US10134289B2 (en) | 2016-02-18 | 2018-11-20 | Honeywell International Inc. | Methods and systems facilitating stabilized descent to a diversion airport |
US9884690B2 (en) | 2016-05-03 | 2018-02-06 | Honeywell International Inc. | Methods and systems for conveying destination viability |
FR3053781B1 (fr) * | 2016-07-07 | 2018-08-17 | Thales | Procede de calcul par un systeme de gestion de vol d'une trajectoire presentant des transitions ameliorees |
FR3053780B1 (fr) * | 2016-07-07 | 2018-07-06 | Thales | Dispositif et methode de calcul de prediction de performance de navigation requise |
US10109203B2 (en) | 2016-09-07 | 2018-10-23 | Honeywell International Inc. | Methods and systems for presenting en route diversion destinations |
US10540899B2 (en) | 2016-11-21 | 2020-01-21 | Honeywell International Inc. | Flight plan segmentation for en route diversion destinations |
US10654589B2 (en) * | 2017-03-27 | 2020-05-19 | Honeywell International Inc. | Avionic display systems and methods for generating vertical situation displays including instability prediction and avoidance symbology |
US10839701B2 (en) | 2018-06-05 | 2020-11-17 | Honeywell International Inc. | Methods and systems for stabilized approach energy management |
US10854091B2 (en) | 2018-07-03 | 2020-12-01 | Honeywell International Inc. | Energy management visualization methods and systems |
US11733712B2 (en) * | 2020-07-03 | 2023-08-22 | Honeywell International Inc. | Systems and methods for generating displays for noise abatement departure procedures |
Family Cites Families (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4021009A (en) * | 1975-07-24 | 1977-05-03 | Sperry Rand Corporation | Vertical path control for aircraft area navigation system |
US5070458A (en) * | 1989-03-31 | 1991-12-03 | Honeywell Inc. | Method of analyzing and predicting both airplane and engine performance characteristics |
US6691004B2 (en) * | 1995-07-31 | 2004-02-10 | Honeywell International, Inc. | Method for determining a currently obtainable climb gradient of an aircraft |
US7064680B2 (en) * | 2002-12-20 | 2006-06-20 | Aviation Communications & Surveillance Systems Llc | Aircraft terrain warning systems and methods |
FR2852683B1 (fr) * | 2003-03-19 | 2005-05-20 | Airbus France | Procede et dispositif d'aide au pilotage d'un aeronef lors d'une approche de non precision pendant une phase d'atterrissage. |
FR2864269B1 (fr) * | 2003-12-19 | 2006-04-07 | Thales Sa | Procede d'aide a la navigation a basse altitude d'un aeronef |
FR2878060B1 (fr) * | 2004-11-15 | 2010-11-05 | Airbus France | Procede et dispositif d'alerte et d'evitement de terrain pour un aeronef |
US9057627B2 (en) * | 2005-03-15 | 2015-06-16 | Fci Associates, Inc. | Low cost flight instrumentation system |
FR2887065B1 (fr) * | 2005-06-14 | 2007-07-20 | Airbus France Sas | Procede et systeme d'aide au pilotage d'un aeronef volant a basse altitude |
US20070078600A1 (en) * | 2005-09-20 | 2007-04-05 | Honeywell International Inc. | System and method of collision avoidance using an invarient set based on vehicle states and dynamic characteristics |
FR2893146B1 (fr) * | 2005-11-10 | 2008-01-25 | Thales Sa | Systeme d'evitement de terrain pour aeronefs de transport |
FR2897976B1 (fr) * | 2006-02-28 | 2008-10-17 | Airbus France Sas | Procede et dispositif d'assistance au pilotage d'un aeronef. |
ES2324561T5 (es) * | 2007-02-23 | 2012-10-19 | The Boeing Company | Implementación de aproximaciones de descenso continuo para máxima previsibilidad en aeronaves |
US7729263B2 (en) * | 2007-08-08 | 2010-06-01 | Honeywell International Inc. | Aircraft data link network routing |
US8761970B2 (en) * | 2008-10-21 | 2014-06-24 | The Boeing Company | Alternative method to determine the air mass state of an aircraft and to validate and augment the primary method |
ATE528705T1 (de) * | 2009-02-25 | 2011-10-15 | Boeing Co | Implementierung kontinuierlicher landeanflüge für maximale vorhersagbarkeit bei flugzeugen |
US9058040B2 (en) * | 2009-02-27 | 2015-06-16 | The Boeing Company | Automatic pilot pitch angle compensation |
-
2009
- 2009-09-04 FR FR0904211A patent/FR2949897B1/fr active Active
-
2010
- 2010-09-07 US US12/876,952 patent/US8849478B2/en active Active
Also Published As
Publication number | Publication date |
---|---|
FR2949897A1 (fr) | 2011-03-11 |
US8849478B2 (en) | 2014-09-30 |
US20110082605A1 (en) | 2011-04-07 |
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Legal Events
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