FR2992072B1 - Procede de pilotage automatique de l'axe de lacet pour aeronef a commandes de vol mecaniques - Google Patents

Procede de pilotage automatique de l'axe de lacet pour aeronef a commandes de vol mecaniques

Info

Publication number
FR2992072B1
FR2992072B1 FR1201716A FR1201716A FR2992072B1 FR 2992072 B1 FR2992072 B1 FR 2992072B1 FR 1201716 A FR1201716 A FR 1201716A FR 1201716 A FR1201716 A FR 1201716A FR 2992072 B1 FR2992072 B1 FR 2992072B1
Authority
FR
France
Prior art keywords
lacet
automatically controlled
flight control
control aircraft
axis method
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
FR1201716A
Other languages
English (en)
Other versions
FR2992072A1 (fr
Inventor
Yannick Meret
Arnaud Bonnaffoux
Christophe Simon
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.)
Thales SA
Original Assignee
Thales SA
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 Thales SA filed Critical Thales SA
Priority to FR1201716A priority Critical patent/FR2992072B1/fr
Priority to US13/917,487 priority patent/US8812178B2/en
Priority to IT000489A priority patent/ITTO20130489A1/it
Priority to RU2013127298/08A priority patent/RU2013127298A/ru
Publication of FR2992072A1 publication Critical patent/FR2992072A1/fr
Application granted granted Critical
Publication of FR2992072B1 publication Critical patent/FR2992072B1/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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/02—Initiating means
    • B64C13/16—Initiating means actuated automatically, e.g. responsive to gust detectors
    • B64C13/18—Initiating means actuated automatically, e.g. responsive to gust detectors using automatic pilot

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Mechanical Engineering (AREA)
  • Steering Control In Accordance With Driving Conditions (AREA)
FR1201716A 2012-06-15 2012-06-15 Procede de pilotage automatique de l'axe de lacet pour aeronef a commandes de vol mecaniques Active FR2992072B1 (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
FR1201716A FR2992072B1 (fr) 2012-06-15 2012-06-15 Procede de pilotage automatique de l'axe de lacet pour aeronef a commandes de vol mecaniques
US13/917,487 US8812178B2 (en) 2012-06-15 2013-06-13 Method for automatic yaw axis control for aircraft with mechanical flight controls
IT000489A ITTO20130489A1 (it) 2012-06-15 2013-06-13 Metodo per il controllo automatico dell'asse di imbardata per un aeromobile con comandi di volo meccanici.
RU2013127298/08A RU2013127298A (ru) 2012-06-15 2013-06-14 Способ автоматического управления по каналу рысканья для летательного аппарата с механическими элементами управления полетом

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1201716A FR2992072B1 (fr) 2012-06-15 2012-06-15 Procede de pilotage automatique de l'axe de lacet pour aeronef a commandes de vol mecaniques

Publications (2)

Publication Number Publication Date
FR2992072A1 FR2992072A1 (fr) 2013-12-20
FR2992072B1 true FR2992072B1 (fr) 2016-07-22

Family

ID=47049206

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1201716A Active FR2992072B1 (fr) 2012-06-15 2012-06-15 Procede de pilotage automatique de l'axe de lacet pour aeronef a commandes de vol mecaniques

Country Status (4)

Country Link
US (1) US8812178B2 (fr)
FR (1) FR2992072B1 (fr)
IT (1) ITTO20130489A1 (fr)
RU (1) RU2013127298A (fr)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2993858B1 (fr) * 2012-07-27 2014-08-22 Thales Sa Procede de regulation en couple d'un actionneur de gouverne commande en position angulaire d'un aeronef a commande de vol mecanique
WO2016105650A1 (fr) * 2014-11-05 2016-06-30 Tzafrir Sheffer Système de pilote automatique, et composants et procédés associés
US11104421B2 (en) 2014-11-05 2021-08-31 Tzafrir Sheffer Autopilot system, and related components and methods
US10005561B2 (en) * 2016-06-16 2018-06-26 Ge Aviation Systems Llc Controlling aircraft using thrust differential trim
KR20240074811A (ko) * 2021-09-29 2024-05-28 투사스- 투르크 하바즐릭 베 유제이 사나이 아노님 시르케티 트림 탭 제어 장치

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3018071A (en) * 1957-08-01 1962-01-23 Lear Inc Trim control system for autopilots
US4479620A (en) * 1978-07-13 1984-10-30 The Boeing Company Wing load alleviation system using tabbed allerons
US4992713A (en) * 1988-10-11 1991-02-12 Rockwell International Corporation Aircraft autopilot with yaw control by rudder force
US7021587B1 (en) * 2004-01-07 2006-04-04 Trutrak Flight Systems, Inc Dual channel fail-safe system and method for adjusting aircraft trim
FR2908107B1 (fr) * 2006-11-06 2008-12-19 Airbus France Sa Procede et dispositif pour estimer les forces s'exercant sur une surface de controle d'un aeronef.
US20100102173A1 (en) * 2008-10-21 2010-04-29 Everett Michael L Light Aircraft Stabilization System
FR2948628B1 (fr) * 2009-08-03 2012-02-03 Airbus Operations Sas Avion a controle en lacet par trainee differentielle
US8718839B2 (en) * 2009-12-06 2014-05-06 Evolved Aircraft Systems, L.L.C. Method and apparatus for automatically controlling aircraft flight control trim systems

Also Published As

Publication number Publication date
US20130345907A1 (en) 2013-12-26
FR2992072A1 (fr) 2013-12-20
ITTO20130489A1 (it) 2013-12-16
RU2013127298A (ru) 2014-12-20
US8812178B2 (en) 2014-08-19

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