FR2371725A1 - Dispositif automatique de stabilisation de la direction d'avions roulant au sol - Google Patents
Dispositif automatique de stabilisation de la direction d'avions roulant au solInfo
- Publication number
- FR2371725A1 FR2371725A1 FR7734348A FR7734348A FR2371725A1 FR 2371725 A1 FR2371725 A1 FR 2371725A1 FR 7734348 A FR7734348 A FR 7734348A FR 7734348 A FR7734348 A FR 7734348A FR 2371725 A1 FR2371725 A1 FR 2371725A1
- Authority
- FR
- France
- Prior art keywords
- automatic steering
- stabilization device
- steering stabilization
- sensor
- present
- 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.)
- Granted
Links
- 230000006641 stabilisation Effects 0.000 title abstract 2
- 238000011105 stabilization Methods 0.000 title abstract 2
- 238000005096 rolling process Methods 0.000 abstract 1
Classifications
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- G05D1/0083—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots to help an aircraft pilot in the rolling phase
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Automation & Control Theory (AREA)
- Regulating Braking Force (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
La présente invention concerne un dispositif automatique de stabilisation de la direction destiné aux avions roulant au sol, et notamment au processus de roulement à l'atterrissage. La présente invention propose un capteur qui enregistre les déviations de l'avion par rapport à sa direction, avec un transducteur dont le signal de sortie est fonction de la différence entre la valeur effective enregistrée par le capteur et la valeur de consigne pré-établie par la direction, et peut être transmis en tant qu'ordre de direction à des organes ou dispositifs de direction.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE2652289A DE2652289C2 (de) | 1976-11-17 | 1976-11-17 | Automatisches Richtungsstabilisierungssystem |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2371725A1 true FR2371725A1 (fr) | 1978-06-16 |
FR2371725B1 FR2371725B1 (fr) | 1983-02-04 |
Family
ID=5993333
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR7734348A Granted FR2371725A1 (fr) | 1976-11-17 | 1977-11-15 | Dispositif automatique de stabilisation de la direction d'avions roulant au sol |
Country Status (5)
Country | Link |
---|---|
US (1) | US4221350A (fr) |
DE (1) | DE2652289C2 (fr) |
FR (1) | FR2371725A1 (fr) |
GB (1) | GB1591271A (fr) |
IT (1) | IT1088241B (fr) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2009115224A1 (fr) * | 2008-03-18 | 2009-09-24 | Airbus France | Procede et dispositif de pilotage lateral d'un aeronef roulant au sol |
Families Citing this family (22)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3135117A1 (de) * | 1980-09-05 | 1982-04-01 | Mitsubishi Denki K.K., Tokyo | Roboterfahrzeug |
US4464661A (en) * | 1982-02-18 | 1984-08-07 | The Ltv Aerospace And Defense Company | System monitor circuit having first and second phase-sensitive demodulator circuits coupled to first and second loads, and a comparator section for monitoring the loads |
US6604708B1 (en) * | 1989-12-26 | 2003-08-12 | The Boeing Company | Carbon brake wear for aircraft |
US6241325B1 (en) | 1997-10-14 | 2001-06-05 | The Boeing Company | Low-speed antiskid control for multigain hydraulic valve brake system |
US6142585A (en) * | 1997-10-14 | 2000-11-07 | The Boeing Company | Antiskid/autobrake control system with low-speed brake release to reduce gear walk |
US6671588B2 (en) * | 2001-12-27 | 2003-12-30 | Toyota Jidosha Kabushiki Kaisha | System and method for controlling traveling direction of aircraft |
US6641085B1 (en) * | 2002-10-04 | 2003-11-04 | Triumph Brands, Inc. | Self-centering steering module |
US6851649B1 (en) | 2003-08-14 | 2005-02-08 | The Boeing Company | Methods and systems for controlling wheel brakes on aircraft and other vehicles |
US7357357B2 (en) * | 2004-03-12 | 2008-04-15 | Airbus Uk Limited | Aircraft mode suppression |
US7281684B2 (en) * | 2005-02-23 | 2007-10-16 | The Boeing Company | Systems and methods for braking aircraft, including braking intermediate main gears and differential braking |
FR2887222B1 (fr) * | 2005-06-15 | 2007-08-10 | Airbus France Sas | Procede et dispositif pour la conduite d'un aeronef roulant sur le sol |
GB0702332D0 (en) | 2007-02-07 | 2007-03-21 | Airbus Uk Ltd | A method, apparatus or software for controlling the heading of an aircraft on the ground |
JP5073424B2 (ja) * | 2007-09-05 | 2012-11-14 | 住友精密工業株式会社 | 航空機の地上操向装置及び地上操向方法 |
NL2001846C2 (nl) * | 2008-07-22 | 2010-01-25 | Robertus Gerardus De Boer | Automatische reminrichting voor een vliegtuig bij dwarswindoperaties. |
US20100102173A1 (en) * | 2008-10-21 | 2010-04-29 | Everett Michael L | Light Aircraft Stabilization System |
US9216720B2 (en) | 2009-04-30 | 2015-12-22 | Goodrich Corporation | Differential emergency/park electric brake system |
JP5608918B2 (ja) * | 2009-06-22 | 2014-10-22 | 独立行政法人 宇宙航空研究開発機構 | 航空機のステアリング角制御システム |
FR2975376B1 (fr) * | 2011-05-20 | 2018-03-30 | Safran Landing Systems | Procede pour alimenter des moteurs de deplacement autonome d'un aeronef. |
GB2540182A (en) * | 2015-07-08 | 2017-01-11 | Airbus Operations Ltd | Aircraft steering system controller |
US10300897B2 (en) * | 2017-05-15 | 2019-05-28 | Goodrich Corporation | Brake load balance and runway centering techniques |
CN110697031A (zh) * | 2019-10-24 | 2020-01-17 | 中国航空工业集团公司沈阳飞机设计研究所 | 一种飞机前轮偏转角度控制系统 |
CN114013636B (zh) * | 2021-11-02 | 2023-02-10 | 西安航空制动科技有限公司 | 一种飞机机轮刹车系统防滑失效分析及仿真的方法 |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2674331A (en) * | 1952-01-23 | 1954-04-06 | Stanford R Ovshinsky | Automatic steering control apparatus for self-propelled vehicles |
GB811300A (en) * | 1955-06-01 | 1959-04-02 | Dunlop Rubber Co | Braking system for aircraft |
FR1298041A (fr) * | 1961-08-03 | 1962-07-06 | Bliss E W Co | Système de guidage terrestre pour véhicules |
US3107514A (en) * | 1961-12-26 | 1963-10-22 | Sperry Rand Corp | Aircraft heading alignment apparatus and method |
US3757887A (en) * | 1971-07-09 | 1973-09-11 | Versadyne Inc | Vehicle guidance system |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1045252B (de) * | 1937-03-19 | 1958-11-27 | Ambi Budd Presswerk Ges Mit Be | Rahmen, insbesondere fuer Kraftfahrzeuge |
US2953323A (en) * | 1955-12-06 | 1960-09-20 | Houdaille Industries Inc | Two-stage steering control system for aircraft nosewheel |
GB1182268A (en) * | 1966-11-17 | 1970-02-25 | Elliott Brothers London Ltd | Improvements in or relating to Aircraft Control Systems. |
US3711042A (en) * | 1970-07-13 | 1973-01-16 | Na Sa | Aircraft control system |
US3823899A (en) * | 1972-10-20 | 1974-07-16 | Lockheed Aircraft Corp | Actuation system for angularly positioning aircraft landing gear wheels |
JPS5310334B2 (fr) * | 1973-03-01 | 1978-04-13 | ||
US4006870A (en) * | 1973-12-26 | 1977-02-08 | The Boeing Company | Self-aligning roll out guidance system |
US3919961A (en) * | 1974-04-17 | 1975-11-18 | John A Mcdougal | Autopilot system |
US4008868A (en) * | 1975-12-18 | 1977-02-22 | The United States Of America As Represented By The Secretary Of The Navy | Aircraft steering and braking system |
-
1976
- 1976-11-17 DE DE2652289A patent/DE2652289C2/de not_active Expired
-
1977
- 1977-11-11 GB GB47115/77A patent/GB1591271A/en not_active Expired
- 1977-11-14 US US05/850,904 patent/US4221350A/en not_active Expired - Lifetime
- 1977-11-15 FR FR7734348A patent/FR2371725A1/fr active Granted
- 1977-11-15 IT IT29666/77A patent/IT1088241B/it active
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2674331A (en) * | 1952-01-23 | 1954-04-06 | Stanford R Ovshinsky | Automatic steering control apparatus for self-propelled vehicles |
GB811300A (en) * | 1955-06-01 | 1959-04-02 | Dunlop Rubber Co | Braking system for aircraft |
FR1298041A (fr) * | 1961-08-03 | 1962-07-06 | Bliss E W Co | Système de guidage terrestre pour véhicules |
US3107514A (en) * | 1961-12-26 | 1963-10-22 | Sperry Rand Corp | Aircraft heading alignment apparatus and method |
US3757887A (en) * | 1971-07-09 | 1973-09-11 | Versadyne Inc | Vehicle guidance system |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2009115224A1 (fr) * | 2008-03-18 | 2009-09-24 | Airbus France | Procede et dispositif de pilotage lateral d'un aeronef roulant au sol |
FR2929019A1 (fr) * | 2008-03-18 | 2009-09-25 | Airbus France Sas | Procede et dispositif de pilotage lateral d'un aeronef roulant au sol. |
Also Published As
Publication number | Publication date |
---|---|
US4221350A (en) | 1980-09-09 |
DE2652289A1 (de) | 1978-05-18 |
GB1591271A (en) | 1981-06-17 |
FR2371725B1 (fr) | 1983-02-04 |
DE2652289C2 (de) | 1983-02-03 |
IT1088241B (it) | 1985-06-10 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |