DE60303272D1 - Flugzeugsteuerungssystem und -verfahren - Google Patents

Flugzeugsteuerungssystem und -verfahren

Info

Publication number
DE60303272D1
DE60303272D1 DE60303272T DE60303272T DE60303272D1 DE 60303272 D1 DE60303272 D1 DE 60303272D1 DE 60303272 T DE60303272 T DE 60303272T DE 60303272 T DE60303272 T DE 60303272T DE 60303272 D1 DE60303272 D1 DE 60303272D1
Authority
DE
Germany
Prior art keywords
piloting
aircraft
law
derivative
order
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 - Lifetime
Application number
DE60303272T
Other languages
English (en)
Other versions
DE60303272T2 (de
Inventor
Stomegaphane Walter
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
Publication of DE60303272D1 publication Critical patent/DE60303272D1/de
Application granted granted Critical
Publication of DE60303272T2 publication Critical patent/DE60303272T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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
DE60303272T 2002-06-12 2003-05-27 Flugzeugsteuerungssystem und -verfahren Expired - Lifetime DE60303272T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0207197A FR2841008B1 (fr) 2002-06-12 2002-06-12 Procede et systeme de pilotage d'un aeronef
FR0207197 2002-06-12

Publications (2)

Publication Number Publication Date
DE60303272D1 true DE60303272D1 (de) 2006-04-06
DE60303272T2 DE60303272T2 (de) 2006-09-14

Family

ID=29559144

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60303272T Expired - Lifetime DE60303272T2 (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
US6935596B2 (en) 2005-08-30
EP1372053A1 (de) 2003-12-17
CA2429861C (fr) 2013-11-19
ATE316262T1 (de) 2006-02-15
CA2429861A1 (fr) 2003-12-12
FR2841008B1 (fr) 2004-08-20
FR2841008A1 (fr) 2003-12-19
DE60303272T2 (de) 2006-09-14
US20050151024A1 (en) 2005-07-14
EP1372053B1 (de) 2006-01-18

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