FR2909463B1 - Procede et dispositif de controle actif du roulis d'un avion - Google Patents

Procede et dispositif de controle actif du roulis d'un avion

Info

Publication number
FR2909463B1
FR2909463B1 FR0610595A FR0610595A FR2909463B1 FR 2909463 B1 FR2909463 B1 FR 2909463B1 FR 0610595 A FR0610595 A FR 0610595A FR 0610595 A FR0610595 A FR 0610595A FR 2909463 B1 FR2909463 B1 FR 2909463B1
Authority
FR
France
Prior art keywords
aircraft
roll
active control
active
control
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
FR0610595A
Other languages
English (en)
Other versions
FR2909463A1 (fr
Inventor
Fabrice Villaume
David Chabe
Stephane Delannoy
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 FR0610595A priority Critical patent/FR2909463B1/fr
Priority to US11/949,233 priority patent/US7908043B2/en
Publication of FR2909463A1 publication Critical patent/FR2909463A1/fr
Application granted granted Critical
Publication of FR2909463B1 publication Critical patent/FR2909463B1/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 or altitude of land, water, air, or space vehicles, e.g. automatic pilot
    • G05D1/0083—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot to help an aircraft pilot in the rolling phase
FR0610595A 2006-12-05 2006-12-05 Procede et dispositif de controle actif du roulis d'un avion Active FR2909463B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR0610595A FR2909463B1 (fr) 2006-12-05 2006-12-05 Procede et dispositif de controle actif du roulis d'un avion
US11/949,233 US7908043B2 (en) 2006-12-05 2007-12-03 Method and device for active control of the roll of an aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0610595A FR2909463B1 (fr) 2006-12-05 2006-12-05 Procede et dispositif de controle actif du roulis d'un avion

Publications (2)

Publication Number Publication Date
FR2909463A1 FR2909463A1 (fr) 2008-06-06
FR2909463B1 true FR2909463B1 (fr) 2014-07-18

Family

ID=38337852

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0610595A Active FR2909463B1 (fr) 2006-12-05 2006-12-05 Procede et dispositif de controle actif du roulis d'un avion

Country Status (2)

Country Link
US (1) US7908043B2 (fr)
FR (1) FR2909463B1 (fr)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2924831B1 (fr) * 2007-12-11 2010-11-19 Airbus France Procede et dispositif de generation d'un ordre de vitesse de lacet pour un aeronef roulant au sol
US9463868B2 (en) 2015-01-06 2016-10-11 Textron Innovations Inc. Systems and methods for aircraft control surface hardover and disconnect protection
FR3032551B1 (fr) 2015-02-09 2020-11-06 Airbus Operations Sas Systeme et procede de pilotage d'un aeronef.
RU2601032C1 (ru) * 2015-09-29 2016-10-27 Федеральное государственное унитарное предприятие "Московское опытно-конструкторское бюро "Марс" (ФГУП МОКБ "Марс") Способ формирования сигнала угловой стабилизации по крену летательного аппарата с оценкой и компенсацией внешнего возмущения и устройство для его осуществления
RU2601089C1 (ru) * 2015-09-29 2016-10-27 Федеральное государственное унитарное предприятие "Московское опытно-конструкторское бюро "Марс" (ФГУП МОКБ "Марс") Способ формирования нелинейного адаптивного цифроаналогового сигнала стабилизации углового положения беспилотного летательного аппарата и система стабилизации для его осуществления
RU2631736C1 (ru) * 2016-09-16 2017-09-26 Федеральное государственное унитарное предприятие "Московское опытно-конструкторское бюро "Марс" (ФГУП МОКБ "Марс") Способ формирования сигнала управления боковым движением нестационарного беспилотного летательного аппарата с адаптивно-функциональной коррекцией и устройство для его осуществления
RU2650307C1 (ru) * 2017-02-14 2018-04-11 Акционерное общество "Военно-промышленная корпорация "Научно-производственное объединение машиностроения" Способ формирования адаптивного сигнала управления боковым движением летательного аппарата
RU2653409C1 (ru) * 2017-07-10 2018-05-08 Федеральное государственное унитарное предприятие "Московское опытно-конструкторское бюро "Марс" (ФГУП МОКБ "Марс") Способ формирования цифроаналогового сигнала угловой стабилизации нестационарного объекта управления и устройство для его осуществления

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4460858A (en) * 1982-05-11 1984-07-17 The Boeing Company Autopilot roll control wheel steering system
US5008825A (en) * 1989-05-01 1991-04-16 Nadkarni Arun A Apparatus and methods for automatically maintaining aircraft track angle
FR2874204B1 (fr) 2004-08-13 2007-12-14 Airbus France Sas Systeme de commande de vol electriques pour les gouvernes de profondeur d'un aeronef

Also Published As

Publication number Publication date
US20080133071A1 (en) 2008-06-05
FR2909463A1 (fr) 2008-06-06
US7908043B2 (en) 2011-03-15

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