JP2010519653A5 - - Google Patents
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- Publication number
- JP2010519653A5 JP2010519653A5 JP2009551024A JP2009551024A JP2010519653A5 JP 2010519653 A5 JP2010519653 A5 JP 2010519653A5 JP 2009551024 A JP2009551024 A JP 2009551024A JP 2009551024 A JP2009551024 A JP 2009551024A JP 2010519653 A5 JP2010519653 A5 JP 2010519653A5
- Authority
- JP
- Japan
- Prior art keywords
- aircraft
- descent
- flight
- type
- ground speed
- 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.)
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Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| EP07380053A EP1962256B2 (en) | 2007-02-23 | 2007-02-23 | Continuous descent approaches for maximum predictability |
| EP07380053.4 | 2007-02-23 | ||
| PCT/US2008/054663 WO2008118581A2 (en) | 2007-02-23 | 2008-02-22 | Implementing continuous descent approaches for maximum predictability in aircraft |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JP2010519653A JP2010519653A (ja) | 2010-06-03 |
| JP2010519653A5 true JP2010519653A5 (enExample) | 2011-04-07 |
| JP5256218B2 JP5256218B2 (ja) | 2013-08-07 |
Family
ID=38190021
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2009551024A Active JP5256218B2 (ja) | 2007-02-23 | 2008-02-22 | 航空機を誘導する方法、航空機を管理する方法、及び、航空機管理システム |
Country Status (9)
| Country | Link |
|---|---|
| US (1) | US8655506B2 (enExample) |
| EP (1) | EP1962256B2 (enExample) |
| JP (1) | JP5256218B2 (enExample) |
| AT (1) | ATE430352T1 (enExample) |
| AU (1) | AU2008231236B2 (enExample) |
| CA (1) | CA2674732C (enExample) |
| DE (1) | DE602007001023D1 (enExample) |
| ES (1) | ES2324561T5 (enExample) |
| WO (1) | WO2008118581A2 (enExample) |
Families Citing this family (25)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| ES2371321T3 (es) * | 2009-02-25 | 2011-12-29 | The Boeing Company | Puesta en práctica de aproximaciones de descenso continuo para máxima previsibilidad en una aeronave. |
| 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. |
| US8311687B2 (en) * | 2010-07-30 | 2012-11-13 | Ge Aviation Systems Llc | Method and system for vertical navigation using time-of-arrival control |
| US9934692B2 (en) * | 2012-02-22 | 2018-04-03 | Honeywell International Inc. | Display system and method for generating a display |
| US8645009B2 (en) * | 2012-02-23 | 2014-02-04 | Ge Aviation Systems Llc | Method for flying an aircraft along a flight path |
| US8653990B2 (en) * | 2012-06-18 | 2014-02-18 | The Boeing Company | Stall management system |
| US9026275B1 (en) * | 2013-07-24 | 2015-05-05 | Shih-Yih Young | In-flight generation of RTA-compliant optimal profile descent paths |
| FR3012598B1 (fr) * | 2013-10-25 | 2016-02-26 | Thales Sa | Procede et systeme de gestion de vol |
| FR3014213B1 (fr) * | 2013-12-04 | 2016-02-05 | Airbus Operations Sas | Procede et dispositif de determination automatique d'un profil de vitesse a paliers de vitesse pour un aeronef. |
| JP6431732B2 (ja) * | 2014-09-19 | 2018-11-28 | 株式会社エヌ・ティ・ティ・データ | 着陸支援装置、航空管制システム、及び着陸支援方法 |
| US10152195B2 (en) | 2015-12-14 | 2018-12-11 | Honeywell International Inc. | Aircraft display system pertaining to energy management |
| US10096252B2 (en) | 2016-06-29 | 2018-10-09 | General Electric Company | Methods and systems for performance based arrival and sequencing and spacing |
| US10388171B2 (en) * | 2017-02-15 | 2019-08-20 | Honeywell International Inc. | Cockpit display systems and methods for generating cockpit displays including direct approach energy management symbology |
| 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 |
| FR3065567B1 (fr) * | 2017-04-24 | 2021-04-16 | Airbus Operations Sas | Procede de transmission de parametres de vol d'un aeronef meneur vers un aeronef intrus |
| CN107991552A (zh) * | 2017-11-20 | 2018-05-04 | 中国运载火箭技术研究院 | 一种重复使用运载器寿命评估及预测系统及方法 |
| US10847044B2 (en) | 2018-02-28 | 2020-11-24 | Honeywell International Inc. | Systems and methods for presenting graphical display elements for variable or adaptive aircraft glideslope and safe areas for aircraft operations |
| 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 |
| 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) |
| US11358733B2 (en) * | 2020-01-21 | 2022-06-14 | Rockwell Collins, Inc. | Optimum idle descent start point display based on current conditions |
| US11842629B2 (en) * | 2020-12-10 | 2023-12-12 | Honeywell International Inc. | Dynamic radar vectoring guidance methods and systems |
| US20240427349A1 (en) * | 2023-01-06 | 2024-12-26 | The Boeing Company | System and Methods for Operating an Aircraft During a Climb Phase of Flight |
| CN116755473B (zh) * | 2023-08-18 | 2023-11-07 | 四川腾盾科技有限公司 | 一种翼吊运输无人机空投任务规划方法 |
Family Cites Families (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4825374A (en) * | 1985-12-20 | 1989-04-25 | The Boeing Company | Aircraft descent guide system and method for creating descent guidance information |
| US4792906A (en) * | 1986-08-29 | 1988-12-20 | The Boeing Company | Navigational apparatus and methods for displaying aircraft position with respect to a selected vertical flight path profile |
| US5225829A (en) * | 1991-05-09 | 1993-07-06 | Sundstrand Corporation | Independent low airspeed alert |
| US7611098B2 (en) * | 2005-01-19 | 2009-11-03 | Airbus France | Flight management process for an aircraft |
| US8027758B2 (en) * | 2005-01-19 | 2011-09-27 | Airbus Operations (S.A.S.) | Navigation system for an aircraft and associated command process |
| TWM284120U (en) * | 2005-05-18 | 2005-12-21 | Time Technology Ind Co Ltd F | Improved structure of a coaxial connector |
| FR2915304B1 (fr) * | 2007-04-20 | 2009-06-05 | Thales Sa | Procede de calcul de trajectoire d'approche pour aeronef |
| ES2371321T3 (es) * | 2009-02-25 | 2011-12-29 | The Boeing Company | Puesta en práctica de aproximaciones de descenso continuo para máxima previsibilidad en una aeronave. |
-
2007
- 2007-02-23 ES ES07380053T patent/ES2324561T5/es active Active
- 2007-02-23 DE DE602007001023T patent/DE602007001023D1/de active Active
- 2007-02-23 AT AT07380053T patent/ATE430352T1/de not_active IP Right Cessation
- 2007-02-23 EP EP07380053A patent/EP1962256B2/en active Active
-
2008
- 2008-02-22 US US12/526,099 patent/US8655506B2/en active Active
- 2008-02-22 AU AU2008231236A patent/AU2008231236B2/en active Active
- 2008-02-22 WO PCT/US2008/054663 patent/WO2008118581A2/en not_active Ceased
- 2008-02-22 CA CA2674732A patent/CA2674732C/en active Active
- 2008-02-22 JP JP2009551024A patent/JP5256218B2/ja active Active
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