FR2570201B1 - Procede de commande d'un aerodyne a moteur, tel qu'avion, en phase de montee adapte a optimiser le cout d'exploitation dudit aerodyne - Google Patents

Procede de commande d'un aerodyne a moteur, tel qu'avion, en phase de montee adapte a optimiser le cout d'exploitation dudit aerodyne

Info

Publication number
FR2570201B1
FR2570201B1 FR8413836A FR8413836A FR2570201B1 FR 2570201 B1 FR2570201 B1 FR 2570201B1 FR 8413836 A FR8413836 A FR 8413836A FR 8413836 A FR8413836 A FR 8413836A FR 2570201 B1 FR2570201 B1 FR 2570201B1
Authority
FR
France
Prior art keywords
aerodyne
aircraft
optimize
controlling
motor
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.)
Expired
Application number
FR8413836A
Other languages
English (en)
Other versions
FR2570201A1 (fr
Inventor
Dominique Berger
Vincent Rivron
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.)
Airbus Group SAS
Original Assignee
Airbus Group 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 Airbus Group SAS filed Critical Airbus Group SAS
Priority to FR8413836A priority Critical patent/FR2570201B1/fr
Priority to DE19853531711 priority patent/DE3531711A1/de
Priority to GB08522150A priority patent/GB2164765B/en
Priority to US06/773,813 priority patent/US4827417A/en
Publication of FR2570201A1 publication Critical patent/FR2570201A1/fr
Application granted granted Critical
Publication of FR2570201B1 publication Critical patent/FR2570201B1/fr
Expired legal-status Critical Current

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
    • G05D1/04—Control of altitude or depth
    • G05D1/06—Rate of change of altitude or depth
    • G05D1/0607—Rate of change of altitude or depth specially adapted for aircraft
    • 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

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)
  • Combined Controls Of Internal Combustion Engines (AREA)
  • Feedback Control In General (AREA)
FR8413836A 1984-09-10 1984-09-10 Procede de commande d'un aerodyne a moteur, tel qu'avion, en phase de montee adapte a optimiser le cout d'exploitation dudit aerodyne Expired FR2570201B1 (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
FR8413836A FR2570201B1 (fr) 1984-09-10 1984-09-10 Procede de commande d'un aerodyne a moteur, tel qu'avion, en phase de montee adapte a optimiser le cout d'exploitation dudit aerodyne
DE19853531711 DE3531711A1 (de) 1984-09-10 1985-09-05 Verfahren zur steuerung eines motorluftfahrzeuges wie eines flugzeugs in aufstiegsphase zur optimierung der betriebskosten dieses luftfahrzeugs
GB08522150A GB2164765B (en) 1984-09-10 1985-09-06 A method of controlling an engine aerodyne in the climb phase
US06/773,813 US4827417A (en) 1984-09-10 1985-09-09 Control method for optimizing exploitation costs of an engine aerodyne such as aircraft in the climb phase

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8413836A FR2570201B1 (fr) 1984-09-10 1984-09-10 Procede de commande d'un aerodyne a moteur, tel qu'avion, en phase de montee adapte a optimiser le cout d'exploitation dudit aerodyne

Publications (2)

Publication Number Publication Date
FR2570201A1 FR2570201A1 (fr) 1986-03-14
FR2570201B1 true FR2570201B1 (fr) 1987-01-09

Family

ID=9307557

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8413836A Expired FR2570201B1 (fr) 1984-09-10 1984-09-10 Procede de commande d'un aerodyne a moteur, tel qu'avion, en phase de montee adapte a optimiser le cout d'exploitation dudit aerodyne

Country Status (4)

Country Link
US (1) US4827417A (fr)
DE (1) DE3531711A1 (fr)
FR (1) FR2570201B1 (fr)
GB (1) GB2164765B (fr)

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GB2211965B (en) * 1987-10-31 1992-05-06 Rolls Royce Plc Data processing systems
US5121325A (en) * 1990-04-04 1992-06-09 Smiths Industries Aerospace & Defense Systems, Inc. Required time of arrival (RTA) control system
US5235512A (en) * 1991-06-24 1993-08-10 Ford Motor Company Self-tuning speed control for a vehicle
US5483448A (en) * 1992-12-14 1996-01-09 Ford Motor Company Adaptive vehicle suspension system with mechanism for varying controller gains in response to changing road roughness conditions
US5574647A (en) * 1993-10-04 1996-11-12 Honeywell Inc. Apparatus and method for computing wind-sensitive optimum altitude steps in a flight management system
US5760712A (en) * 1996-09-04 1998-06-02 American Circuit Technology, Inc. Fuel time indicator
US20030176954A1 (en) * 2001-10-12 2003-09-18 Jaw Link C. Tracking and control of gas turbine engine component damage/life
FR2894705B1 (fr) * 2005-12-13 2010-11-19 Thales Sa Systeme de gestion de vol d'un aeronef
US7337058B1 (en) * 2007-02-12 2008-02-26 Honeywell International, Inc. Engine wear characterizing and quantifying method
US7606658B2 (en) * 2007-09-12 2009-10-20 Honeywell International Inc. Financial decision aid for 4-D navigation
FR2939917B1 (fr) * 2008-12-12 2012-09-21 Thales Sa Procede et dispositif pour l'optimisation du vol d'un aeronef
US9646114B2 (en) * 2013-07-10 2017-05-09 The Boeing Company Electrical power system stability
FR3019912B1 (fr) * 2014-04-10 2016-05-13 Safety Line Systeme et procede de determination des parametres de vol et de la consommation en carburant d'au moins une phase de vol d'un avion
FR3046268B1 (fr) * 2015-12-23 2019-05-10 Safran Aircraft Engines Systeme d'exploitation de donnees de vol d'un aeronef
US10579053B2 (en) * 2016-09-08 2020-03-03 Ge Aviation Systems, Llc Aircraft control based on fuel, time, and deterioration costs
US20190005826A1 (en) 2017-06-28 2019-01-03 Ge Aviation Systems, Llc Engine load model systems and methods

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4038526A (en) * 1967-12-29 1977-07-26 The Secretary Of State For Defence In Her Britanic Majesty's Government Of The United Kingdom Of Great Britain And Northern Ireland Optimizing control system for aircraft
CH584940A5 (fr) * 1974-08-07 1977-02-15 Soechtig Gerhard
US3958107A (en) * 1974-12-09 1976-05-18 Edelson Andrew C Fuel management computer
US4032093A (en) * 1975-06-27 1977-06-28 The Boeing Company Adaptive energy management for vertical speed control of an aircraft
US4019702A (en) * 1975-11-13 1977-04-26 The Boeing Company Method and apparatus for guiding a jet aircraft in a noise-abated post-takeoff climb
US4159088A (en) * 1977-01-03 1979-06-26 The Boeing Company System for reducing aircraft fuel consumption
US4312041A (en) * 1978-02-22 1982-01-19 Lear Siegler, Inc. Flight performance data computer system
US4325123A (en) * 1978-07-28 1982-04-13 The Boeing Company Economy performance data avionic system
US4347572A (en) * 1979-11-02 1982-08-31 The Boeing Company Method and apparatus for an aircraft climb-out guidance system
US4357663A (en) * 1979-12-03 1982-11-02 The Boeing Company Method and apparatus for aircraft pitch and thrust axes control
US4445179A (en) * 1980-03-07 1984-04-24 Michelotti Paul E Aircraft minimum drag speed system
US4326253A (en) * 1980-03-31 1982-04-20 The Boeing Company Lift control system for aircraft vertical path guidance
US4577275A (en) * 1983-05-31 1986-03-18 United Technologies Corporation Flight director go-around mode

Also Published As

Publication number Publication date
GB2164765A (en) 1986-03-26
GB8522150D0 (en) 1985-10-09
DE3531711C2 (fr) 1990-03-29
DE3531711A1 (de) 1986-04-17
GB2164765B (en) 1987-12-02
FR2570201A1 (fr) 1986-03-14
US4827417A (en) 1989-05-02

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