DE602004020022D1 - Einstellvorrichtung für mindestens einen Parameter, insbesondere für ein Autopilotsystem eines Flugzeuges - Google Patents

Einstellvorrichtung für mindestens einen Parameter, insbesondere für ein Autopilotsystem eines Flugzeuges

Info

Publication number
DE602004020022D1
DE602004020022D1 DE602004020022T DE602004020022T DE602004020022D1 DE 602004020022 D1 DE602004020022 D1 DE 602004020022D1 DE 602004020022 T DE602004020022 T DE 602004020022T DE 602004020022 T DE602004020022 T DE 602004020022T DE 602004020022 D1 DE602004020022 D1 DE 602004020022D1
Authority
DE
Germany
Prior art keywords
aircraft
parameter
adjusting device
units
detects
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
DE602004020022T
Other languages
English (en)
Inventor
Stephane Granger
Thierry Bourret
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 DE602004020022D1 publication Critical patent/DE602004020022D1/de
Anticipated expiration legal-status Critical
Active legal-status Critical Current

Links

Classifications

    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
    • G05B9/00—Safety arrangements
    • G05B9/02—Safety arrangements electric
    • G05B9/03—Safety arrangements electric with multiple-channel loop, i.e. redundant control systems
DE602004020022T 2003-05-19 2004-05-05 Einstellvorrichtung für mindestens einen Parameter, insbesondere für ein Autopilotsystem eines Flugzeuges Active DE602004020022D1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0305948A FR2855281B1 (fr) 2003-05-19 2003-05-19 Dispositif de reglage d'au moins un parametre, en particulier d'un systeme de pilotage automatique d'un aeronef.

Publications (1)

Publication Number Publication Date
DE602004020022D1 true DE602004020022D1 (de) 2009-04-30

Family

ID=33396547

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602004020022T Active DE602004020022D1 (de) 2003-05-19 2004-05-05 Einstellvorrichtung für mindestens einen Parameter, insbesondere für ein Autopilotsystem eines Flugzeuges

Country Status (6)

Country Link
US (1) US7400949B2 (de)
EP (1) EP1491975B1 (de)
AT (1) ATE426196T1 (de)
CA (1) CA2469822C (de)
DE (1) DE602004020022D1 (de)
FR (1) FR2855281B1 (de)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2855281B1 (fr) * 2003-05-19 2005-08-05 Airbus France Dispositif de reglage d'au moins un parametre, en particulier d'un systeme de pilotage automatique d'un aeronef.
WO2020044134A1 (en) * 2018-08-29 2020-03-05 H55 Sa Aircraft monitoring system and method for electric or hybrid aircrafts

Family Cites Families (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4368618A (en) * 1980-10-02 1983-01-18 The Bendix Corporation Manually operated metering valve for a fuel control
JPS5811810A (ja) * 1981-07-14 1983-01-22 Matsushita Electric Ind Co Ltd サイクルタイマ−装置
US4517161A (en) * 1982-09-29 1985-05-14 Grumman Aerospace Corp. Combustible vapor detection system
JP2786893B2 (ja) * 1989-07-21 1998-08-13 豊田工機株式会社 砥石の研削先端点の座標位置検出方法
JPH04216344A (ja) * 1990-12-18 1992-08-06 Matsushita Electric Ind Co Ltd 映像再生装置
US5920170A (en) * 1992-10-08 1999-07-06 Yamanashi Numerical control apparatus and numerical control method
JPH0730589A (ja) * 1993-07-06 1995-01-31 Canon Inc データ送信装置
US7103460B1 (en) * 1994-05-09 2006-09-05 Automotive Technologies International, Inc. System and method for vehicle diagnostics
US5602333A (en) * 1994-06-17 1997-02-11 Smiths Industries Apparatus for measuring the level of a liquid in a tank
US5621666A (en) * 1995-04-20 1997-04-15 Dynavisions, Inc. Planter monitor
IL117792A (en) * 1995-05-08 2003-10-31 Rafael Armament Dev Authority Autonomous command and control unit for mobile platform
US5663732A (en) * 1995-05-25 1997-09-02 Honeywell Inc. Integrity monitoring method and apparatus for GPS and DGPS receivers
FR2753171B1 (fr) * 1996-09-09 1998-11-13 Aerospatiale Dispositif de controle de la poussee d'un aeronef a plusieurs moteurs
JP2000078281A (ja) * 1998-09-01 2000-03-14 Seiko Epson Corp 電源オンの携帯型移動電話機の検知システム
US6227492B1 (en) * 1999-08-06 2001-05-08 Bell Helicopter Textron Inc. Redundant ice management system for aircraft
US6526337B2 (en) * 2000-03-29 2003-02-25 Conrad O. Gardner Supervisory control system for aircraft flight management during pilot command errors or equipment malfunction
US6446911B1 (en) * 2000-07-14 2002-09-10 Honeywell International Inc. Method for controlling actuators on a vehicle
JP4141860B2 (ja) * 2003-02-26 2008-08-27 健蔵 野波 小型無人ヘリコプタの自律制御装置及びプログラム
FR2855281B1 (fr) * 2003-05-19 2005-08-05 Airbus France Dispositif de reglage d'au moins un parametre, en particulier d'un systeme de pilotage automatique d'un aeronef.

Also Published As

Publication number Publication date
US20040236480A1 (en) 2004-11-25
ATE426196T1 (de) 2009-04-15
FR2855281A1 (fr) 2004-11-26
FR2855281B1 (fr) 2005-08-05
US7400949B2 (en) 2008-07-15
EP1491975A3 (de) 2005-04-27
EP1491975B1 (de) 2009-03-18
CA2469822A1 (fr) 2004-11-19
EP1491975A2 (de) 2004-12-29
CA2469822C (fr) 2012-04-17

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