ATE316262T1 - Flugzeugsteuerungssystem und -verfahren - Google Patents

Flugzeugsteuerungssystem und -verfahren

Info

Publication number
ATE316262T1
ATE316262T1 AT03291257T AT03291257T ATE316262T1 AT E316262 T1 ATE316262 T1 AT E316262T1 AT 03291257 T AT03291257 T AT 03291257T AT 03291257 T AT03291257 T AT 03291257T AT E316262 T1 ATE316262 T1 AT E316262T1
Authority
AT
Austria
Prior art keywords
piloting
aircraft
law
derivative
order
Prior art date
Application number
AT03291257T
Other languages
English (en)
Inventor
Stephane Walter
Original Assignee
Airbus France
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 France filed Critical Airbus France
Application granted granted Critical
Publication of ATE316262T1 publication Critical patent/ATE316262T1/de

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
    • G05D1/08—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
AT03291257T 2002-06-12 2003-05-27 Flugzeugsteuerungssystem und -verfahren ATE316262T1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0207197A FR2841008B1 (fr) 2002-06-12 2002-06-12 Procede et systeme de pilotage d'un aeronef

Publications (1)

Publication Number Publication Date
ATE316262T1 true ATE316262T1 (de) 2006-02-15

Family

ID=29559144

Family Applications (1)

Application Number Title Priority Date Filing Date
AT03291257T ATE316262T1 (de) 2002-06-12 2003-05-27 Flugzeugsteuerungssystem und -verfahren

Country Status (6)

Country Link
US (1) US6935596B2 (de)
EP (1) EP1372053B1 (de)
AT (1) ATE316262T1 (de)
CA (1) CA2429861C (de)
DE (1) DE60303272T2 (de)
FR (1) FR2841008B1 (de)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2903379B1 (fr) * 2006-07-07 2008-08-29 Thales Sa Convertisseur de commande de facteur de charge en consigne d'ecart d'assiette longitudinale
US8165733B2 (en) * 2007-09-04 2012-04-24 Embraer S.A. Stall, buffeting, low speed and high attitude protection system
US8342445B2 (en) 2008-09-26 2013-01-01 The Boeing Company Horizontal tail load alleviation system
US8583293B2 (en) * 2009-11-09 2013-11-12 Honeywell International Inc. Flight control surface actuation force fight mitigation system and method
FR3050177B1 (fr) * 2016-04-19 2021-06-25 Airbus Operations Sas Systeme et procede de commande de la poussee des moteurs d'un aeronef

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2044389A5 (de) * 1969-05-19 1971-02-19 Equip Naviga Aerie
US3848833A (en) * 1972-07-14 1974-11-19 Sperry Rand Corp Aircraft automatic flight control system
US4011440A (en) * 1975-04-29 1977-03-08 General Electric Company System for generating an angular rate signal from an angular position signal utilizing a constant amplitude-variable carrier phase signal
US4032094A (en) * 1976-05-19 1977-06-28 Rockwell International Corporation Control of positioning system authority over aircraft control surfaces as a function of surface movement rate
US4209734A (en) * 1978-03-27 1980-06-24 Sperry Corporation Dynamic equalization system for dual channel automatic pilot
DE3928456A1 (de) * 1989-08-29 1991-03-07 Nord Micro Elektronik Feinmech Verfahren und schaltungsanordnung zum bilden eines auswertungssignals aus einer mehrzahl redundanter messsignale
FR2668750B1 (fr) * 1990-11-06 1993-01-22 Aerospatiale Systeme pour la commande integree en profondeur et en poussee d'un aeronef.
US5197697A (en) * 1991-02-08 1993-03-30 Rockwell International Corporation Fly by wire/fly by light control system with manual override
US5722620A (en) * 1995-05-15 1998-03-03 The Boeing Company Aircraft pitch-axis stability and command augmentation
US5615119A (en) * 1995-06-07 1997-03-25 Aurora Flight Sciences Corporation Fault tolerant automatic control system utilizing analytic redundancy
FR2756541B1 (fr) * 1996-12-02 1999-01-22 Aerospatiale Procede pour la protection d'un aeronef contre les rafales de vent vertical et dispositif de pilotage en profondeur mettant en oeuvre ce procede
FR2832123B1 (fr) * 2001-11-14 2004-10-29 Eurocopter France Systeme de commande de vol, pour commander le tangage d'un aeronef a decollage vertical et a direction de portance orientable

Also Published As

Publication number Publication date
CA2429861A1 (fr) 2003-12-12
FR2841008A1 (fr) 2003-12-19
CA2429861C (fr) 2013-11-19
EP1372053B1 (de) 2006-01-18
US6935596B2 (en) 2005-08-30
US20050151024A1 (en) 2005-07-14
DE60303272D1 (de) 2006-04-06
EP1372053A1 (de) 2003-12-17
FR2841008B1 (fr) 2004-08-20
DE60303272T2 (de) 2006-09-14

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Legal Events

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RER Ceased as to paragraph 5 lit. 3 law introducing patent treaties