ATE528705T1 - Implementierung kontinuierlicher landeanflüge für maximale vorhersagbarkeit bei flugzeugen - Google Patents

Implementierung kontinuierlicher landeanflüge für maximale vorhersagbarkeit bei flugzeugen

Info

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
Application number
AT09380031T
Other languages
English (en)
Inventor
David Garrido-Lopez
Ledesma Ramon Gomez
Original Assignee
Boeing Co
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Boeing Co filed Critical Boeing Co
Application granted granted Critical
Publication of ATE528705T1 publication Critical patent/ATE528705T1/de

Links

Classifications

    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/04Control of altitude or depth
    • G05D1/06Rate of change of altitude or depth
    • G05D1/0607Rate of change of altitude or depth specially adapted for aircraft
    • G05D1/0653Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing
    • G05D1/0676Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing specially adapted for landing
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/80Energy 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)
AT09380031T 2009-02-25 2009-02-25 Implementierung kontinuierlicher landeanflüge für maximale vorhersagbarkeit bei flugzeugen ATE528705T1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP09380031A EP2224305B1 (de) 2009-02-25 2009-02-25 Implementierung kontinuierlicher Landeanflüge für maximale Vorhersagbarkeit bei Flugzeugen

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 (de)
EP (1) EP2224305B1 (de)
JP (1) JP5473672B2 (de)
AT (1) ATE528705T1 (de)
ES (1) ES2371321T3 (de)

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EP1962256B2 (de) * 2007-02-23 2012-06-20 The Boeing Company Gleitanflugverfahren für maximale Vorhersagbarkeit
EP2282247B1 (de) * 2009-05-05 2019-07-10 The Boeing Company Vierdimensionale Lenkung eines Flugzeugs
FR2949897B1 (fr) * 2009-09-04 2012-08-03 Thales Sa Procede d'assistance au pilotage d'un aeronef et dispositif correspondant.
EP2423773B1 (de) * 2010-08-24 2014-06-25 The Boeing Company Vierdimensionale Lenkung eines Flugzeugs
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
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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
CN107004369A (zh) 2014-11-05 2017-08-01 霍尼韦尔国际公司 使用程序轨迹预测的空中交通系统
US9418561B2 (en) 2014-12-02 2016-08-16 Honeywell International Inc. System and method for displaying predictive conformal configuration cues for executing a landing
EP3109724B1 (de) 2015-06-26 2022-02-09 The Boeing Company Verfahren und system zur steuerung eines flugs eines flugzeugs mit einer ankunftszeitbeschränkung
EP3385812B1 (de) 2015-06-26 2020-10-14 The Boeing Company Verfahren und system zur steuerung des fluges eines flugzeuges mit mindestens zwei erforderlichen ankunftszeitbeschränkungen
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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Also Published As

Publication number Publication date
JP5473672B2 (ja) 2014-04-16
EP2224305A1 (de) 2010-09-01
JP2010195392A (ja) 2010-09-09
US8442707B2 (en) 2013-05-14
ES2371321T3 (es) 2011-12-29
EP2224305B1 (de) 2011-10-12
US20100217461A1 (en) 2010-08-26

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