FR2931563B1 - Procede et systeme de pilotage permettant l'elimination d'oscillations de couplage oscillatoire - Google Patents

Procede et systeme de pilotage permettant l'elimination d'oscillations de couplage oscillatoire

Info

Publication number
FR2931563B1
FR2931563B1 FR0802727A FR0802727A FR2931563B1 FR 2931563 B1 FR2931563 B1 FR 2931563B1 FR 0802727 A FR0802727 A FR 0802727A FR 0802727 A FR0802727 A FR 0802727A FR 2931563 B1 FR2931563 B1 FR 2931563B1
Authority
FR
France
Prior art keywords
removal
control system
oscillatory coupling
coupling oscillations
oscillations
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
FR0802727A
Other languages
English (en)
Other versions
FR2931563A1 (fr
Inventor
Pierre Fabre
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 FR0802727A priority Critical patent/FR2931563B1/fr
Priority to US12/467,180 priority patent/US8095252B2/en
Publication of FR2931563A1 publication Critical patent/FR2931563A1/fr
Application granted granted Critical
Publication of FR2931563B1 publication Critical patent/FR2931563B1/fr
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
    • G05D1/08—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)
  • Feedback Control In General (AREA)
  • Control Of Electric Motors In General (AREA)
FR0802727A 2008-05-20 2008-05-20 Procede et systeme de pilotage permettant l'elimination d'oscillations de couplage oscillatoire Active FR2931563B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR0802727A FR2931563B1 (fr) 2008-05-20 2008-05-20 Procede et systeme de pilotage permettant l'elimination d'oscillations de couplage oscillatoire
US12/467,180 US8095252B2 (en) 2008-05-20 2009-05-15 Piloting method and device avoiding the pilot induced oscillations

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0802727A FR2931563B1 (fr) 2008-05-20 2008-05-20 Procede et systeme de pilotage permettant l'elimination d'oscillations de couplage oscillatoire

Publications (2)

Publication Number Publication Date
FR2931563A1 FR2931563A1 (fr) 2009-11-27
FR2931563B1 true FR2931563B1 (fr) 2010-06-04

Family

ID=40551541

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0802727A Active FR2931563B1 (fr) 2008-05-20 2008-05-20 Procede et systeme de pilotage permettant l'elimination d'oscillations de couplage oscillatoire

Country Status (2)

Country Link
US (1) US8095252B2 (fr)
FR (1) FR2931563B1 (fr)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10482783B2 (en) 2015-11-06 2019-11-19 Frasca International, Inc. Adaptive assistance for flight simulation
US10906632B2 (en) 2018-05-23 2021-02-02 Bell Helicopter Textron Inc. Systems and methods for controlled filtering of aircraft control input

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4298833A (en) * 1980-02-29 1981-11-03 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Apparatus for damping operator induced oscillations of a controlled system
US5935177A (en) * 1997-02-06 1999-08-10 Accurate Automation Corporation Pilot-induced oscillation detection and compensation apparatus and method
FR2847353B1 (fr) 2002-11-18 2006-07-14 Airbus France Procede et dispositif pour la detection de couplages oscillatoires de pilotage dans un aeronef

Also Published As

Publication number Publication date
US8095252B2 (en) 2012-01-10
US20090292410A1 (en) 2009-11-26
FR2931563A1 (fr) 2009-11-27

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Legal Events

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Effective date: 20110916

CD Change of name or company name

Owner name: AIRBUS HOLDING, FR

Effective date: 20110916

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Effective date: 20110916

TP Transmission of property

Owner name: AIRBUS HOLDING, FR

Effective date: 20110913

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