AU2002217244A1 - Method and device for automatic control of an aircraft deceleration in running phase - Google Patents
Method and device for automatic control of an aircraft deceleration in running phaseInfo
- Publication number
- AU2002217244A1 AU2002217244A1 AU2002217244A AU1724402A AU2002217244A1 AU 2002217244 A1 AU2002217244 A1 AU 2002217244A1 AU 2002217244 A AU2002217244 A AU 2002217244A AU 1724402 A AU1724402 A AU 1724402A AU 2002217244 A1 AU2002217244 A1 AU 2002217244A1
- Authority
- AU
- Australia
- Prior art keywords
- automatic control
- running phase
- aircraft deceleration
- deceleration
- aircraft
- 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.)
- Abandoned
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/42—Arrangement or adaptation of brakes
- B64C25/426—Braking devices providing an automatic sequence of braking
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0016147 | 2000-12-12 | ||
FR0016147A FR2817979B1 (en) | 2000-12-12 | 2000-12-12 | METHOD AND DEVICE FOR AUTOMATICALLY CONTROLLING THE DECELERATION OF AN AIRCRAFT IN RUNNING PHASE |
PCT/FR2001/003923 WO2002047977A1 (en) | 2000-12-12 | 2001-12-11 | Method and device for automatic control of an aircraft deceleration in running phase |
Publications (1)
Publication Number | Publication Date |
---|---|
AU2002217244A1 true AU2002217244A1 (en) | 2002-06-24 |
Family
ID=8857539
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
AU2002217244A Abandoned AU2002217244A1 (en) | 2000-12-12 | 2001-12-11 | Method and device for automatic control of an aircraft deceleration in running phase |
Country Status (7)
Country | Link |
---|---|
US (1) | US6991304B2 (en) |
EP (1) | EP1349779B1 (en) |
AU (1) | AU2002217244A1 (en) |
CA (1) | CA2431361C (en) |
DE (1) | DE60104904T2 (en) |
FR (1) | FR2817979B1 (en) |
WO (1) | WO2002047977A1 (en) |
Families Citing this family (34)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2857468B1 (en) * | 2003-07-08 | 2005-09-30 | Airbus France | SYSTEM FOR AIDING THE CONTROL OF THE DECELERATION OF AN AIRCRAFT RUNNING ON THE GROUND |
GB0405614D0 (en) * | 2004-03-12 | 2004-04-21 | Airbus Uk Ltd | Advanced braking system |
EP1732796B1 (en) * | 2004-03-12 | 2013-01-23 | Airbus Operations Limited | Advanced braking system for aircraft |
NO320851B1 (en) * | 2004-04-15 | 2006-02-06 | Oddvard Johnsen | Brake control functions based on a control for variations in acceleration values in the horizontal plane of the wheel |
FR2895726B1 (en) * | 2006-01-03 | 2009-10-23 | Thales Sa | SYSTEM AND METHOD FOR ASSISTING THE BRAKING OF AN AIRCRAFT ON A LANDING TRAIL |
US7626513B2 (en) * | 2006-08-02 | 2009-12-01 | The Boeing Company | Communication of landing conditions |
US7586422B2 (en) * | 2006-08-02 | 2009-09-08 | The Boeing Company | Determination of runway landing conditions |
US7720579B2 (en) * | 2006-12-20 | 2010-05-18 | The Boeing Company | Method, system, and computer program product for performance monitored aircraft rejected takeoff braking |
FR2914097B1 (en) * | 2007-03-20 | 2014-05-23 | Airbus France | METHOD AND DEVICE FOR AIDING THE CONTROL OF AN AIRCRAFT DURING A LANDING PHASE |
US7818100B2 (en) * | 2007-04-03 | 2010-10-19 | The Boeing Company | System and method for optimized runway exiting |
FR2918637B1 (en) * | 2007-07-09 | 2010-01-29 | Airbus France | EQUALIZATION SYSTEM FOR BRAKING ENERGY. |
US7835845B2 (en) * | 2007-08-23 | 2010-11-16 | Gm Global Technology Operations, Inc. | Method and system for consistent braking control |
FR2924831B1 (en) * | 2007-12-11 | 2010-11-19 | Airbus France | METHOD AND DEVICE FOR GENERATING A LACET SPEED ORDER FOR A GROUNDING AIRCRAFT |
FR2924832B1 (en) | 2007-12-11 | 2010-11-19 | Airbus France | METHOD AND APPARATUS FOR GENERATING A CONTROLLED SPEED FOR AN AIRCRAFT RUNNING ON THE GROUND |
US8060261B2 (en) | 2008-05-21 | 2011-11-15 | The Boeing Company | Method and system of determining effectiveness of an aircraft braking system on an aircraft during an aircraft landing |
FR2936077B1 (en) * | 2008-09-16 | 2014-12-12 | Airbus France | METHOD AND DEVICE FOR AIDING THE CONTROL OF AN AIRCRAFT DURING A LANDING PHASE. |
FR2936078B1 (en) * | 2008-09-16 | 2014-12-12 | Airbus France | METHOD AND DEVICE FOR AIDING THE CONTROL OF AN AIRCRAFT DURING A LANDING PHASE. |
FR2941554B1 (en) * | 2009-01-29 | 2011-04-01 | Airbus France | METHOD AND DEVICE FOR AIDING THE CONTROL OF AN AIRCRAFT DURING A LANDING PHASE |
SE534642C2 (en) * | 2010-02-10 | 2011-11-01 | Vdii Innovation Ab | Method and apparatus for assessing deceleration of a vehicle |
US8560150B1 (en) | 2010-07-07 | 2013-10-15 | The Boeing Company | Methods and systems for landing decision point |
FR2985977B1 (en) * | 2012-01-24 | 2015-01-23 | Airbus Operations Sas | METHOD AND DEVICE FOR AIDING THE CONTROL OF AN AIRCRAFT DURING A LANDING PHASE. |
US9164505B1 (en) | 2012-05-22 | 2015-10-20 | The Boeing Company | Automatic rejected takeoff system |
US9254363B2 (en) | 2012-07-17 | 2016-02-09 | Elwha Llc | Unmanned device interaction methods and systems |
US9125987B2 (en) | 2012-07-17 | 2015-09-08 | Elwha Llc | Unmanned device utilization methods and systems |
US9663223B1 (en) | 2013-02-11 | 2017-05-30 | The Boeing Company | Aircraft braking performance and runway condition determination |
US9340300B2 (en) * | 2013-09-16 | 2016-05-17 | The Boeing Company | On-ground braking alerts for airplanes |
US9082301B2 (en) * | 2013-10-28 | 2015-07-14 | The Boeing Company | Aircraft stopping performance display and warning |
US20150127196A1 (en) * | 2013-11-06 | 2015-05-07 | Honeywell International Inc. | System and method for alerting of remaining runway upon landing based on deceleration |
FR3043387B1 (en) * | 2015-11-05 | 2018-06-22 | Airbus (S.A.S.) | METHOD AND SYSTEM FOR BRAKING AN AIRCRAFT |
FR3045197B1 (en) * | 2015-12-11 | 2018-01-26 | Airbus | IMPROVED METHOD AND SYSTEM FOR AIDING THE CONTROL OF AN AIRCRAFT IN THE LANDING PHASE |
US10814842B2 (en) * | 2016-12-28 | 2020-10-27 | Hydro-Aire, Inc. | System and method for simplified aircraft brake distance estimation |
FR3108582B1 (en) * | 2020-03-27 | 2024-03-22 | Safran Aircraft Engines | SYSTEM FOR MANAGING THE DECELERATION OF AN AIRCRAFT ON A GROUND RUNWAY AND ASSOCIATED METHOD |
FR3111846A1 (en) * | 2020-06-26 | 2021-12-31 | Airbus Operations | METHOD AND DEVICE FOR ESTIMATING THE CONDITION OR PRESSURE OF THE TIRES OF AN AIRCRAFT |
CN112874495A (en) * | 2021-03-02 | 2021-06-01 | 北京航空航天大学 | Aircraft landing braking distance control method |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3920282A (en) * | 1973-09-06 | 1975-11-18 | Boeing Co | Aircraft automatic braking system |
US5024491A (en) * | 1976-11-18 | 1991-06-18 | The Boeing Company | Automatic aircraft braking system including wheelspeed responsive control apparatus |
FR2372058A1 (en) * | 1976-11-29 | 1978-06-23 | Messier Hispano Sa | AUTOMATIC BRAKING METHOD AND DEVICE FOR VEHICLES, ESPECIALLY FOR AIRCRAFT |
EP0025614A1 (en) * | 1979-07-23 | 1981-03-25 | The Boeing Company | Method and apparatus for continuously determining an interval of time during which an action must be taken |
US4454582A (en) * | 1979-07-23 | 1984-06-12 | The Boeing Company | Method and apparatus for continuously determining a chronodrasic interval |
US4316252A (en) * | 1979-08-10 | 1982-02-16 | The Boeing Company | Apparatus for determining the position of an aircraft with respect to the runway |
US5142478A (en) * | 1988-09-23 | 1992-08-25 | Crook Mitchell M | Computerized aircraft landing and takeoff system |
EP0505236A3 (en) * | 1991-03-18 | 1994-11-09 | Thomson Csf | Structured neural networks for complex system control |
US6092919A (en) * | 1995-08-01 | 2000-07-25 | Guided Systems Technologies, Inc. | System and method for adaptive control of uncertain nonlinear processes |
US5968106A (en) | 1997-08-05 | 1999-10-19 | The Boeing Company | Aircraft stop-to-position autobrake control system |
US5951122A (en) * | 1997-12-31 | 1999-09-14 | The B.F. Goodrich Company | Antiskid control and wheel lock protection differential reference controller |
-
2000
- 2000-12-12 FR FR0016147A patent/FR2817979B1/en not_active Expired - Lifetime
-
2001
- 2001-12-11 DE DE60104904T patent/DE60104904T2/en not_active Expired - Lifetime
- 2001-12-11 US US10/450,214 patent/US6991304B2/en not_active Expired - Lifetime
- 2001-12-11 CA CA002431361A patent/CA2431361C/en not_active Expired - Lifetime
- 2001-12-11 WO PCT/FR2001/003923 patent/WO2002047977A1/en not_active Application Discontinuation
- 2001-12-11 AU AU2002217244A patent/AU2002217244A1/en not_active Abandoned
- 2001-12-11 EP EP01270460A patent/EP1349779B1/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
US6991304B2 (en) | 2006-01-31 |
DE60104904T2 (en) | 2005-07-14 |
EP1349779B1 (en) | 2004-08-11 |
CA2431361A1 (en) | 2002-06-20 |
EP1349779A1 (en) | 2003-10-08 |
US20040026992A1 (en) | 2004-02-12 |
FR2817979B1 (en) | 2004-02-27 |
CA2431361C (en) | 2009-11-10 |
FR2817979A1 (en) | 2002-06-14 |
DE60104904D1 (en) | 2004-09-16 |
WO2002047977A1 (en) | 2002-06-20 |
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