FR3019912B1 - SYSTEM AND METHOD FOR DETERMINING FLIGHT PARAMETERS AND FUEL CONSUMPTION OF AT LEAST ONE FLIGHT PHASE OF AN AIRCRAFT - Google Patents

SYSTEM AND METHOD FOR DETERMINING FLIGHT PARAMETERS AND FUEL CONSUMPTION OF AT LEAST ONE FLIGHT PHASE OF AN AIRCRAFT

Info

Publication number
FR3019912B1
FR3019912B1 FR1453184A FR1453184A FR3019912B1 FR 3019912 B1 FR3019912 B1 FR 3019912B1 FR 1453184 A FR1453184 A FR 1453184A FR 1453184 A FR1453184 A FR 1453184A FR 3019912 B1 FR3019912 B1 FR 3019912B1
Authority
FR
France
Prior art keywords
flight
aircraft
fuel consumption
determining
parameters
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
Application number
FR1453184A
Other languages
French (fr)
Other versions
FR3019912A1 (en
Inventor
Pierre Jouniaux
Karim Tekkal
Frederic Bonnans
Pierre Martinon
Stephan Maindrault
Cindie Andrieu
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Institut National de Recherche en Informatique et en Automatique INRIA
Safety Line SAS
Original Assignee
Institut National de Recherche en Informatique et en Automatique INRIA
Safety Line SAS
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 Institut National de Recherche en Informatique et en Automatique INRIA, Safety Line SAS filed Critical Institut National de Recherche en Informatique et en Automatique INRIA
Priority to FR1453184A priority Critical patent/FR3019912B1/en
Priority to PCT/EP2015/057556 priority patent/WO2015155202A1/en
Publication of FR3019912A1 publication Critical patent/FR3019912A1/en
Application granted granted Critical
Publication of FR3019912B1 publication Critical patent/FR3019912B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

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
    • G05D1/0005—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with arrangements to save energy
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C21/00—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00
    • G01C21/20—Instruments for performing navigational calculations
    • G—PHYSICS
    • G06—COMPUTING; CALCULATING OR COUNTING
    • G06Q—INFORMATION AND COMMUNICATION TECHNOLOGY [ICT] SPECIALLY ADAPTED FOR ADMINISTRATIVE, COMMERCIAL, FINANCIAL, MANAGERIAL OR SUPERVISORY PURPOSES; SYSTEMS OR METHODS SPECIALLY ADAPTED FOR ADMINISTRATIVE, COMMERCIAL, FINANCIAL, MANAGERIAL OR SUPERVISORY PURPOSES, NOT OTHERWISE PROVIDED FOR
    • G06Q10/00—Administration; Management
    • G06Q10/04—Forecasting or optimisation specially adapted for administrative or management purposes, e.g. linear programming or "cutting stock problem"
    • G06Q10/047—Optimisation of routes or paths, e.g. travelling salesman problem
    • G—PHYSICS
    • G06—COMPUTING; CALCULATING OR COUNTING
    • G06Q—INFORMATION AND COMMUNICATION TECHNOLOGY [ICT] SPECIALLY ADAPTED FOR ADMINISTRATIVE, COMMERCIAL, FINANCIAL, MANAGERIAL OR SUPERVISORY PURPOSES; SYSTEMS OR METHODS SPECIALLY ADAPTED FOR ADMINISTRATIVE, COMMERCIAL, FINANCIAL, MANAGERIAL OR SUPERVISORY PURPOSES, NOT OTHERWISE PROVIDED FOR
    • G06Q10/00—Administration; Management
    • G06Q10/06—Resources, workflows, human or project management; Enterprise or organisation planning; Enterprise or organisation modelling
    • G06Q10/063—Operations research, analysis or management
    • G—PHYSICS
    • G08—SIGNALLING
    • G08G—TRAFFIC CONTROL SYSTEMS
    • G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
    • G08G5/003—Flight plan management
    • G08G5/0034—Assembly of a flight plan

Landscapes

  • Engineering & Computer Science (AREA)
  • Business, Economics & Management (AREA)
  • Human Resources & Organizations (AREA)
  • General Physics & Mathematics (AREA)
  • Physics & Mathematics (AREA)
  • Remote Sensing (AREA)
  • Economics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Strategic Management (AREA)
  • Entrepreneurship & Innovation (AREA)
  • Operations Research (AREA)
  • Quality & Reliability (AREA)
  • Tourism & Hospitality (AREA)
  • Marketing (AREA)
  • General Business, Economics & Management (AREA)
  • Game Theory and Decision Science (AREA)
  • Theoretical Computer Science (AREA)
  • Development Economics (AREA)
  • Automation & Control Theory (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Educational Administration (AREA)
  • Navigation (AREA)
FR1453184A 2014-04-10 2014-04-10 SYSTEM AND METHOD FOR DETERMINING FLIGHT PARAMETERS AND FUEL CONSUMPTION OF AT LEAST ONE FLIGHT PHASE OF AN AIRCRAFT Active FR3019912B1 (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR1453184A FR3019912B1 (en) 2014-04-10 2014-04-10 SYSTEM AND METHOD FOR DETERMINING FLIGHT PARAMETERS AND FUEL CONSUMPTION OF AT LEAST ONE FLIGHT PHASE OF AN AIRCRAFT
PCT/EP2015/057556 WO2015155202A1 (en) 2014-04-10 2015-04-08 System and method for determining flight parameters and fuel consumption of at least one flight phase of an aeroplane

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1453184A FR3019912B1 (en) 2014-04-10 2014-04-10 SYSTEM AND METHOD FOR DETERMINING FLIGHT PARAMETERS AND FUEL CONSUMPTION OF AT LEAST ONE FLIGHT PHASE OF AN AIRCRAFT

Publications (2)

Publication Number Publication Date
FR3019912A1 FR3019912A1 (en) 2015-10-16
FR3019912B1 true FR3019912B1 (en) 2016-05-13

Family

ID=51518872

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1453184A Active FR3019912B1 (en) 2014-04-10 2014-04-10 SYSTEM AND METHOD FOR DETERMINING FLIGHT PARAMETERS AND FUEL CONSUMPTION OF AT LEAST ONE FLIGHT PHASE OF AN AIRCRAFT

Country Status (2)

Country Link
FR (1) FR3019912B1 (en)
WO (1) WO2015155202A1 (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3373272B1 (en) * 2017-03-09 2019-05-15 The Boeing Company Method and electronic device for providing an optimal quantity of aircraft fuel
FR3089624B1 (en) * 2018-12-06 2021-03-05 Airbus Operations Sas Avionics method and system for generating an optimal vertical trajectory
CN110909950A (en) * 2019-11-29 2020-03-24 中国航空工业集团公司沈阳飞机设计研究所 Method and device for optimizing fuel consumption by adopting non-inferior ranking algorithm

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2570201B1 (en) * 1984-09-10 1987-01-09 Aerospatiale METHOD FOR CONTROLLING AN AERODYNE WITH A MOTOR, SUCH AS AN AIRCRAFT, IN THE RISING PHASE ADAPTED TO OPTIMIZE THE OPERATING COST OF SAID AERODYNE
US5121325A (en) * 1990-04-04 1992-06-09 Smiths Industries Aerospace & Defense Systems, Inc. Required time of arrival (RTA) control system
US7647163B2 (en) * 2005-08-04 2010-01-12 The Boeing Company Automated fueling information tracking and fuel hedging
US7641152B2 (en) * 2007-04-13 2010-01-05 The Boeing Company Dynamic adjustment of wing surfaces for variable camber
FR2939917B1 (en) * 2008-12-12 2012-09-21 Thales Sa METHOD AND DEVICE FOR OPTIMIZING THE FLIGHT OF AN AIRCRAFT
US8160759B2 (en) * 2009-01-23 2012-04-17 Flightaware, Llc System and method for optimized flight planning
US8412392B2 (en) * 2010-02-24 2013-04-02 Honeywell International Inc. Methods and systems for displaying predicted downpath parameters in a vertical profile display
EP2667273A1 (en) * 2012-05-24 2013-11-27 The Boeing Company Method for providing a description of aircraft intent using a decomposition of flight intent into constrained flight segments

Also Published As

Publication number Publication date
FR3019912A1 (en) 2015-10-16
WO2015155202A1 (en) 2015-10-15

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