FR2945513B1 - Procede et dispositif d'optimisation des performances d'un aeronef en presence d'une dissymetrie laterale - Google Patents

Procede et dispositif d'optimisation des performances d'un aeronef en presence d'une dissymetrie laterale

Info

Publication number
FR2945513B1
FR2945513B1 FR0902376A FR0902376A FR2945513B1 FR 2945513 B1 FR2945513 B1 FR 2945513B1 FR 0902376 A FR0902376 A FR 0902376A FR 0902376 A FR0902376 A FR 0902376A FR 2945513 B1 FR2945513 B1 FR 2945513B1
Authority
FR
France
Prior art keywords
dissymetry
optimizing
aircraft
performance
side dissymetry
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 - Fee Related
Application number
FR0902376A
Other languages
English (en)
Other versions
FR2945513A1 (fr
Inventor
Pierre Ezerzere
Stephane Puig
Fabien Calderara
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 Operations SAS
Original Assignee
Airbus Operations 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 Operations SAS filed Critical Airbus Operations SAS
Priority to FR0902376A priority Critical patent/FR2945513B1/fr
Priority to US12/780,669 priority patent/US8527116B2/en
Publication of FR2945513A1 publication Critical patent/FR2945513A1/fr
Application granted granted Critical
Publication of FR2945513B1 publication Critical patent/FR2945513B1/fr
Expired - Fee Related 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
    • G05D1/08—Control of attitude, i.e. control of roll, pitch, or yaw
    • G05D1/0808—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
    • G05D1/0816—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft to ensure stability

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)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Feedback Control In General (AREA)
FR0902376A 2009-05-18 2009-05-18 Procede et dispositif d'optimisation des performances d'un aeronef en presence d'une dissymetrie laterale Expired - Fee Related FR2945513B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR0902376A FR2945513B1 (fr) 2009-05-18 2009-05-18 Procede et dispositif d'optimisation des performances d'un aeronef en presence d'une dissymetrie laterale
US12/780,669 US8527116B2 (en) 2009-05-18 2010-05-14 Process and device for optimising the performance of an aircraft in the presence of a lateral dissymmetry

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0902376A FR2945513B1 (fr) 2009-05-18 2009-05-18 Procede et dispositif d'optimisation des performances d'un aeronef en presence d'une dissymetrie laterale

Publications (2)

Publication Number Publication Date
FR2945513A1 FR2945513A1 (fr) 2010-11-19
FR2945513B1 true FR2945513B1 (fr) 2013-02-08

Family

ID=41057558

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0902376A Expired - Fee Related FR2945513B1 (fr) 2009-05-18 2009-05-18 Procede et dispositif d'optimisation des performances d'un aeronef en presence d'une dissymetrie laterale

Country Status (2)

Country Link
US (1) US8527116B2 (fr)
FR (1) FR2945513B1 (fr)

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2946021B1 (fr) * 2009-05-28 2012-09-28 Airbus France Procede et dispositif pour la detection d'une dissymetrie de poussee d'un aeronef lors d'un atterrissage
FR2978858B1 (fr) * 2011-08-01 2013-08-30 Airbus Operations Sas Procede et systeme pour la determination de parametres de vol d'un aeronef
US8718841B2 (en) * 2012-02-14 2014-05-06 Sikorsky Aircraft Corporation Method and system for providing sideslip envelope protection
DE102013101602A1 (de) * 2013-02-18 2014-09-04 Airbus Operations Gmbh Flugzeug mit einem System zum Beeinflussen des Giermoments und ein Verfahren zum Beeinflussen des Giermoments eines Flugzeugs
EP3741679B1 (fr) * 2013-08-28 2021-12-29 Raytheon Technologies Corporation Équilibrage de poussée d'aéronef à multiples moteurs
US9646505B2 (en) 2014-12-23 2017-05-09 Ge Aviation Systems Llc Method of automatically controlling the descent phase of an aircraft using aircraft avionics executing a descent algorithm
US10255818B2 (en) * 2015-02-11 2019-04-09 Aviation Communication & Surveillance Systems, Llc Systems and methods for weather detection and avoidance
US10005561B2 (en) * 2016-06-16 2018-06-26 Ge Aviation Systems Llc Controlling aircraft using thrust differential trim
EP3333082B1 (fr) * 2016-12-12 2020-06-17 Ge Avio S.r.l. Dispositif de mesure de poussée pour système de propulsion
CA2972495C (fr) 2017-06-28 2025-11-18 Airbus Canada Limited Partnership Orientation de derive destinee a un etat non fonctionnel d'un moteur
CN108033025B (zh) * 2017-11-30 2021-05-14 陶文英 一种航空发动机推力控制系统
US10303184B1 (en) * 2017-12-08 2019-05-28 Kitty Hawk Corporation Autonomous takeoff and landing with open loop mode and closed loop mode
CN113791635B (zh) * 2021-08-24 2023-07-25 中国航天科工集团第二研究院 一种飞行器滚转控制方法、系统及电子设备
US11592846B1 (en) 2021-11-10 2023-02-28 Beta Air, Llc System and method for autonomous flight control with mode selection for an electric aircraft
CN116166040B (zh) * 2023-03-07 2026-02-13 中国航空研究院 一种高超声速飞行器横向不对称在线配平控制方法
CN117094078B (zh) * 2023-07-24 2024-12-13 成都飞机工业（集团）有限责任公司 一种侧滑角自适应的横航向控制舵面设计方法

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2617120B1 (fr) * 1987-06-24 1989-12-08 Aerospatiale Systeme pour la commande d'un aeronef en roulis et en lacet
US5170969A (en) * 1988-11-23 1992-12-15 The Boeing Company Aircraft rudder command system
US6561020B2 (en) * 2001-05-08 2003-05-13 Rosemount Aerospace Inc. Method to calculate sideslip angle and correct static pressure for sideslip effects using inertial information
US6594559B2 (en) * 2001-05-08 2003-07-15 Rosemount Aerospace Inc. Iterative method of aircraft sideslip compensation for multi-function probe air data systems
US7606641B2 (en) 2005-08-04 2009-10-20 The Boeing Company Fuel consumption data tracking/collection and aircraft/route optimization
FR2897592B1 (fr) * 2006-02-20 2008-04-04 Airbus France Sas Procede et dispositif de detection d'une dissymetrie laterale d'un aeronef.
US7706932B2 (en) * 2006-11-30 2010-04-27 Instituto Nacional de Tecnica Aeroespacial “Estaban Terradas” Method for controlling control parameters in an air vehicle and system of controlling an air vehicle
NL2002064C (nl) * 2008-10-07 2010-04-08 Robertus Gerardus De Boer Gedifferentieerde stuwkracht startmethode voor een vliegtuig.

Also Published As

Publication number Publication date
US8527116B2 (en) 2013-09-03
FR2945513A1 (fr) 2010-11-19
US20110046823A1 (en) 2011-02-24

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Effective date: 20110916

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