ATE400498T1 - Verfahren und system zum verschieben eines flugzeugseitenruders - Google Patents
Verfahren und system zum verschieben eines flugzeugseitenrudersInfo
- Publication number
- ATE400498T1 ATE400498T1 AT03291892T AT03291892T ATE400498T1 AT E400498 T1 ATE400498 T1 AT E400498T1 AT 03291892 T AT03291892 T AT 03291892T AT 03291892 T AT03291892 T AT 03291892T AT E400498 T1 ATE400498 T1 AT E400498T1
- Authority
- AT
- Austria
- Prior art keywords
- force
- rudder
- moving
- aircraft rudder
- order
- Prior art date
Links
Classifications
-
- 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
- B64C13/24—Transmitting means
- B64C13/38—Transmitting means with power amplification
- B64C13/50—Transmitting means with power amplification using electrical energy
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
Landscapes
- Engineering & Computer Science (AREA)
- Automation & Control Theory (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Control Devices (AREA)
- Regulating Braking Force (AREA)
- Radio Relay Systems (AREA)
- Steering Control In Accordance With Driving Conditions (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0211124A FR2844251B1 (fr) | 2002-09-09 | 2002-09-09 | Procede et systeme pour deplacer une gouverne d'un aeronef. |
Publications (1)
Publication Number | Publication Date |
---|---|
ATE400498T1 true ATE400498T1 (de) | 2008-07-15 |
Family
ID=31503138
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
AT03291892T ATE400498T1 (de) | 2002-09-09 | 2003-07-30 | Verfahren und system zum verschieben eines flugzeugseitenruders |
Country Status (6)
Country | Link |
---|---|
US (1) | US6928340B2 (de) |
EP (1) | EP1396421B1 (de) |
AT (1) | ATE400498T1 (de) |
CA (1) | CA2437216C (de) |
DE (1) | DE60322002D1 (de) |
FR (1) | FR2844251B1 (de) |
Families Citing this family (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7593793B2 (en) * | 2004-07-30 | 2009-09-22 | The Boeing Company | Adaptive control in the presence of input constraints |
FR2891051B1 (fr) * | 2005-09-22 | 2007-10-19 | Airbus France Sas | Procede et dispositif pour realiser au moins un essai en vol sur un aeronef et applications |
FR2892699B1 (fr) * | 2005-10-27 | 2008-02-08 | Airbus France Sas | Procede et systeme de limitation d'un angle de braquage de la gouverne d'un aeronef |
FR2897838B1 (fr) * | 2006-02-27 | 2009-01-09 | Airbus France Sas | Systeme de commande electrique pour une gouverne de direction d'un avion. |
US8245967B2 (en) | 2008-11-25 | 2012-08-21 | The Boeing Company | Actuator force equalization controller |
US8504221B2 (en) * | 2009-01-16 | 2013-08-06 | The Boeing Company | Apparatus and method for controlling a control surface of a vehicle based on a load identified on the control surface |
FR2959575B1 (fr) * | 2010-05-03 | 2014-08-29 | Airbus Operations Sas | Procede et dispositif pour la reduction des charges engendrees sur un avion par une perturbation aerodynamique. |
US9821903B2 (en) * | 2014-07-14 | 2017-11-21 | The Boeing Company | Closed loop control of aircraft control surfaces |
CN109521750B (zh) * | 2018-03-16 | 2021-12-03 | 陕西飞机工业(集团)有限公司 | 一种停机制动操纵系统 |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5170969A (en) * | 1988-11-23 | 1992-12-15 | The Boeing Company | Aircraft rudder command system |
EP0488428A3 (en) * | 1990-09-24 | 1992-10-14 | The Boeing Company | Apparatus and method for reducing aircraft loads resulting from atmospheric turbulence and gusts |
US6539290B1 (en) * | 1995-06-07 | 2003-03-25 | Dabulamanzi Holdings, Llc | Method, apparatus and design procedure for controlling multi-input, multi-output (MIMO) parameter dependent systems using feedback LTI'zation |
US6209825B1 (en) * | 1998-02-27 | 2001-04-03 | Lockheed Martin Corporation | Low power loss electro hydraulic actuator |
FR2793765B1 (fr) * | 1999-05-18 | 2001-07-13 | Eurocopter France | Dispositif de commande de vol d'un aeronef |
FR2809373B1 (fr) | 2000-05-29 | 2002-08-09 | Aerospatiale Matra Airbus | Systeme de commande electrique pour une gouverne de direction d'aeronef |
-
2002
- 2002-09-09 FR FR0211124A patent/FR2844251B1/fr not_active Expired - Fee Related
-
2003
- 2003-07-30 EP EP03291892A patent/EP1396421B1/de not_active Expired - Lifetime
- 2003-07-30 AT AT03291892T patent/ATE400498T1/de not_active IP Right Cessation
- 2003-07-30 DE DE60322002T patent/DE60322002D1/de not_active Expired - Lifetime
- 2003-08-14 CA CA2437216A patent/CA2437216C/fr not_active Expired - Fee Related
- 2003-09-04 US US10/654,621 patent/US6928340B2/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
CA2437216C (fr) | 2011-02-15 |
EP1396421A1 (de) | 2004-03-10 |
US6928340B2 (en) | 2005-08-09 |
FR2844251A1 (fr) | 2004-03-12 |
US20040111190A1 (en) | 2004-06-10 |
CA2437216A1 (fr) | 2004-03-09 |
FR2844251B1 (fr) | 2005-05-27 |
DE60322002D1 (de) | 2008-08-21 |
EP1396421B1 (de) | 2008-07-09 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
RER | Ceased as to paragraph 5 lit. 3 law introducing patent treaties |