JP2010195392A5 - - Google Patents

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Publication number
JP2010195392A5
JP2010195392A5 JP2010039652A JP2010039652A JP2010195392A5 JP 2010195392 A5 JP2010195392 A5 JP 2010195392A5 JP 2010039652 A JP2010039652 A JP 2010039652A JP 2010039652 A JP2010039652 A JP 2010039652A JP 2010195392 A5 JP2010195392 A5 JP 2010195392A5
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JP
Japan
Prior art keywords
ground speed
turn
flight path
path angle
aerodynamic flight
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Application number
JP2010039652A
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English (en)
Japanese (ja)
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JP2010195392A (ja
JP5473672B2 (ja
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Priority claimed from EP09380031A external-priority patent/EP2224305B1/en
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Publication of JP2010195392A publication Critical patent/JP2010195392A/ja
Publication of JP2010195392A5 publication Critical patent/JP2010195392A5/ja
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Publication of JP5473672B2 publication Critical patent/JP5473672B2/ja
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JP2010039652A 2009-02-25 2010-02-25 連続降下アプローチによる航空機の予測可能性の最大化 Active JP5473672B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
EP09380031.6 2009-02-25
EP09380031A EP2224305B1 (en) 2009-02-25 2009-02-25 Implementing continuous descent approaches for maximum predictability in aircraft

Publications (3)

Publication Number Publication Date
JP2010195392A JP2010195392A (ja) 2010-09-09
JP2010195392A5 true JP2010195392A5 (enExample) 2013-04-04
JP5473672B2 JP5473672B2 (ja) 2014-04-16

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ID=41393638

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2010039652A Active JP5473672B2 (ja) 2009-02-25 2010-02-25 連続降下アプローチによる航空機の予測可能性の最大化

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)

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US9442490B2 (en) * 2011-04-29 2016-09-13 Airbus Engineering Centre India System and method for aircraft performance predictions for descent and approach phases
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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

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